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LAPPEENRANTA UNIVERSITY OF TECHNOLOGY Faculty of Technology LUT Energy Electrical Engineering Savelii Zhukov Loss Modelling of Three-Level Inverters controlled with Space Vector Modulation Technique Examiners: Professor Olli Pyrhönen M.Sc. Tatu Musikka Advisors: M.Sc. Raimo Juntunen

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Page 1: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

LAPPEENRANTA UNIVERSITY OF TECHNOLOGY

Faculty of Technology

LUT Energy

Electrical Engineering

Savelii Zhukov

Loss Modelling of Three-Level Inverters controlled with Space Vector Modulation

Technique

Examiners: Professor Olli Pyrhönen

M.Sc. Tatu Musikka

Advisors: M.Sc. Raimo Juntunen

Page 2: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

ABSTRACT

LAPPEENRANTA UNIVERSITY OF TECHNOLOGY

Faculty of Technology

LUT Energy

Electrical Engineering

Savelii Zhukov

Loss Modelling of Three-Level Inverters controlled with Space Vector Modulation

Technique

Master’s Thesis

2012

87 pages, 33 figures, 13 tables and 10 appendices

Examiners: Professor Olli Pyrhönen

M.Sc Tatu Musikka

Keywords: ANPC, Losses, SVM, IGBT, Three-level inverter

The objective of this master’s thesis is to investigate the loss behavior of three-level ANPC

inverter and compare it with conventional NPC inverter. The both inverters are controlled

with mature space vector modulation strategy. In order to provide the comparison both

accurate and detailed enough NPC and ANPC simulation models should be obtained.

The similar control model of SVM is utilized for both NPC and ANPC inverter models. The

principles of control algorithms, the structure and description of models are clarified. The

power loss calculation model is based on practical calculation approaches with certain

assumptions. The comparison between NPC and ANPC topologies is presented based on

results obtained for each semiconductor device, their switching and conduction losses and

efficiency of the inverters.

Alternative switching states of ANPC topology allow distributing losses among the switches

more evenly, than in NPC inverter. Obviously, the losses of a switching device depend on its

position in the topology. Losses distribution among the components in ANPC topology

allows reducing the stress on certain switches, thus losses are equally distributed among the

semiconductors, however the efficiency of the inverters is the same.

As a new contribution to earlier studies, the obtained models of SVM control, NPC and

ANPC inverters have been built. Thus, this thesis can be used in further more complicated

modelling of full-power converters for modern multi-megawatt wind energy conversion

systems.

Page 3: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

ACKNOWLEDGEMENTS

This thesis has been written to Electrical Engineering Department of Lappeenranta

University of Technology in the spring semester 2012 during my studies as a double-degree

student there.

Firstly, I wish announce my gratitude to Professor Olli Pyrhönen. I am thankful to him for

his right path guidance during this work and suggestive comments. I also would like to thank

Dr. Katja Hynynen on the first steps of the work and both Mr. Tatu Musikka and Mr. Raimo

Juntunen for their words of advice, discussions and patience. Without their help in difficult

times it would be much harder to obtain any results, and I appreciate it.

Secondly, I also wish thank my colleagues and people both in Finland and Russia for their

support and understanding during my studies here: Prof. Alexander Mikerov, Dr. Victor

Vtorov, Nikita Potashko, Peter Leshev and Lina Shilkova. I am grateful to you.

Finally, my thanks would be incomplete, if I would not thank my mother Dr. Elvira Zhukova

for her comprehensive support. I appreciate it and I will always be thankful to you.

Page 4: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

TABLE OF CONTENTS

1 INTRODUCTION 7

1.1 WIND ENERGY CONVERSION SYSTEMS 8

1.1.1 Frequency converters in WECS 12

1.2 CONVERTER TOPOLOGIES FOR HIGH POWER APPLICATIONS 13

1.2.1 Three-level Neutral Point Clamped inverter 19

1.2.2 Three-level Active Neutral Point Clamped inverter 22

1.2.3 Switching devices of the inverter 25

2 POWER LOSSES IN THE INVERTER 28

2.1 COMMUTATIONS AND LOSSES IN THREE-LEVEL NPC INVERTER 28

2.2 COMMUTATIONS AND LOSSES IN THREE-LEVEL ANPC INVERTER 32

2.2.1 Loss balancing in three-level ANPC converter 38

2.3 POWER LOSSES OF SEMICONDUCTOR DEVICES 40

2.3.1 IGBT and diode switching losses 44

2.3.2 IGBT and diode conduction losses 45

3 DYNAMIC SIMULATION AND MODULATION PRINCIPLES 49

3.1 MODULATION STRATEGIES FOR MULTILEVEL CONVERTERS 49

3.2 SPACE VECTOR MODULATION OF NPC INVERTER 52

3.2.1. Determination of sector and region of SV 55

3.2.2 Determination of switching states and their sequences 57

3.3.3 Calculating the switching times and durations 62

4 SIMULATION METHODS AND RESULTS 65

Page 5: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

4.1 MODELLING OF THREE-LEVEL INVERTER CONTROLLED WITH SVM 65

4.1.1 SVM control of NPC inverter model 66

4.2 SIMULATION RESULTS FOR NPC AND ANPC INVERTERS 71

4.2.1 Comparison of losses calculation results and efficiency 75

5 SUMMARY AND CONCLUSIONS 78

REFERENCES 80

Page 6: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

LIST OF SYMBOLS

Roman letters

E Energy [J]

f Frequency [Hz]

I, i Current [A]

k Number of base vectors in a sector [-]

L Inductance [H]

m Number of phases [-], Modulation index [-]

N Number of switching states [-]

n Number of voltage levels [-]

P Power loss [W]

R Resistance [Ω]

T, t Time period [s], Switching duration [s]

U Voltage [V]

V Unity voltage vector [-]

Page 7: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

Greek letters

α Phase angle of voltage vector [rad]

ϑ Junction temperature [°C]

Subscripts

av Average value

0 Initial, Default value

b Blocking

CE Collector-emitter

com Commutation

C, cond Conducting, conduction

d Delay, Discretization

DC Direct Current, DC-link parameter

D Diode parameter

f Fall, Fundamental

i Current parameter

IGBT IGBT parameter

in Inner

Page 8: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

LL Line-to-line

load Load parameter

loss Losses

min Minimum

n Nominal,

npc Neutral Point Clamped

off Turn-off state

o, on Turn-on state

out Outer

ph Phase

r Rise

rated Rated value

rec Recovery

ref Reference

RMS Root Mean Square

sec Sector

sw Switching

s Sampling

tol Tolerance

v Voltage parameter

Page 9: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

x Number of phase

LIST OF ABBREVIATIONS

AC Alternating Current

ANPC Active Neutral Point Clamped

CHB Cascade Half Bridge

CSI Current Source Inverter

D Diode

DC Direct Current

DFIG Doubly Fed Induction Generator

DPGS Distributed Power Generation System

FLC Flying Capacitor

G Generator

IGBT Insulated Gate Bipolar Transistor

ML Multi-Level

NPC Neutral Point Clamped

NTV The Nearest Triangle Vector

PEBB Power Electronics Building Blocks

PEC Power Electronics Converter

Page 10: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

PF Power Factor

PMSG Permanent Magnet Synchronous Generator

PWM Pulse-Width Modulation

RMS Root-mean-square

S Switch

SVM Space Vector Modulation

THD Total Harmonic Distortion

VSI Voltage Source Inverter

VSC Voltage Source Converter

VSWT Variable Speed Wind Turbine

WECS Wind Energy Conversion System

WTG Wind Turbine Generator

WWEA World Wind Energy Association

Page 11: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

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1 INTRODUCTION

Nowadays the amount of installed variable speed wind turbines (VSWT) increased, since

the importance of power electronics converters (PECs) performance also becomes crucial,

as PEC provides an interface between wind turbine generator (WTG) and the electrical

grid. In general, the performance of PEC is widely discussed in literature from two points

of view, which are the efficiency of the converter and the quality of output voltages and

currents. These issues become vital for PECs, as the share of energy produced by wind

energy conversion systems (WECS) increases worldwide annually. So, mature and

extensively used two-level topology converters dominating on the market are replaced by

the converters with multi-level (ML) including three-level topology with better

performance. The performance of the three-level inverter as an integral part of the three-

level converter is investigated in this work. As a new contribution to earlier studies, both

simulation models of three-level active neutral point clamped (ANPC) and neutral-point

clamped (NPC) inverters are presented in this study, combined with space vector

modulation (SVM) strategy and simulations in order to adequately assert and compare their

efficiencies.

Thus, the objective of this thesis is to design a simulation model of three-level (ANPC)

inverter with a space vector pulse-width modulation (SVPWM) control module in order to

compare its performance with neutral-point clamped (NPC) inverter. So, a simulation

model of NPC inverter should be also designed.

In general, the thesis comprises four parts with summary and conclusions. The first part is

devoted to frequency converters utilized in wind energy conversion systems, different

topologies of available medium-voltage inverters and their switching devices. In addition,

NPC and ANPC topologies are investigated here in details.

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Power losses occurring in semiconductor devices of the inverter are discussed in the second

part of the thesis. The nature of switching and conduction losses of these components is

investigated here. In addition, methods for losses calculation are also presented in this part.

In the third part of the thesis available modulation strategies are discussed. Attention is

mostly focused on the space-vector modulation (SVM) principle, as exactly this method is

used in simulation models.

In the fourth part simulation models are described as well as obtained results are presented.

The implementation of the utilized SVM principle and techniques of efficiency calculation

are also presented here. The obtained voltage and current curves, as well as calculated

results can be found here. Finally, the summary with discussion of obtained results and

conclusions are presented. The further possible improvements and development of the

models are also discussed here.

1.1 Wind energy conversion systems

Greenhouse effect control has been one of the crucial global challenges, especially for the

last couple decades, when more evidences of global warming had been reported. It is

known that the further greenhouse effect developments can be eliminated only if CO2

emissions are reduced significantly. Recently, the European Commission has announced a

proposal for a new Energy Policy for Europe. One of the issues of the Energy Policy is to

increase the share of renewable energy sources in the overall generation production in order

to decrease CO2 emissions by at least 20% by 2020 and 50% until 2050 (MELICIO et al

2010). So, environmental concerns become extremely relevant for electric companies as

regulations on pollutions become more severe as well.

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Another issue is that in general, it is predicted that prices on fossil fuels will increase

annually in next decades (DECC 2011). In addition, governments of some countries, for

instance in Germany, announced the plan to renounce the nuclear power plants on the

territory of the country or at least drastically reduced its share in electricity generation.

Hence, it is expected that renewable energy sources will be an important part of the future

Energy Policy for Europe. Even nowadays distributed power generation systems (DPGS),

including for instance wind turbines, photovoltaic and solar panels, become an integral part

of modern power generation sector (MELICIO et al 2010).

Among all DPGSs, WECSs are the most mature and rapidly developing technology. Thus,

its annual installation growth rate exceed 30% every year and sets new records, for instance

42 GW of new capacity was installed in 2011. According to the preliminary published data

gathered by World Wind Energy Association (WWEA 2012), the total capacity of wind

power generation reached 239 Gigawatt worldwide in 2011, and it is enough to cover 3 %

of the world's electricity demand already.

Figure 1. Wind power world total installed capacity in GW (WWEA 2012)

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As it can be seen from Fig.2, any modern WECS comprise three integral aspects:

aerodynamic, mechanical and electrical ones. The aim of this kind of the complex system is

to convert motional energy of the wind into electrical power.

Figure 2. Wind energy conversion system general structure (KIM et al 2010)

In this thesis the issues related only to electrical aspect are discussed. Variable-speed wind

energy conversion systems offer the following advantages: mechanical stress is reduced,

torque oscillations are not transmitted to the grid, and below rated wind speed the rotor

speed is controlled to achieve maximum aerodynamic efficiency. Thus, induction

generators or doubly fed induction generators (DFIGs) fully dominate on the variable-speed

WECSs market nowadays (MELICIO et al 2010). However, as alternative for generator

unit of these conventional variable-speed WECSs with DFIGs, modern permanent magnet

synchronous generators (PMSGs) have been introduced recently. Advantages of this

approach can be found in (LAMPOLA 2000). In particular, the whole system structure with

PMSG as a generator unit is presented in Fig.3.

Figure 3. Permanent magnet wind power drive (PYRHONEN et al 2011)

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From the structure scheme in Figure 3 it can be seen clearly that such a directly driven wind

turbine has gearless nature and obviously low speed. In general, in gearless drive multi-pole

low speed high power generators are preferred. In addition, the generator is completely

decoupled from the grid in this variable-speed WECS structure with full-power converter.

One of the advantages of full-power converter wind energy conversion systems is ability to

control active and reactive output power (NALLAVAN et al 2011). The possible converters

structures which are commonly used in wind power applications are considered in the

following chapters.

According to (MELICIO et al 2010; WIZELIUS 2006), in recent years, there has been a

kind of new tendency of wind turbine generators (WTGs) design revealed. Thus, the rotor

size of new WTGs has been significantly increased in order to extract more power from

wind and improve performance of wind energy conversion systems. In general, the cost

structure for wind power applications is based on the fact, that a turbine shares 40-80% of

the whole costs depending on onshore or offshore application. As a turbine comprises both

generator unit and gearbox components, eliminating gearbox and related mechanical

components may be preferable alternative.

In addition, reliability is an important factor for economic efficiency since maintenance and

repair are extremely expensive and not guaranteed at any time, for instance due to difficult

access to the offshore wind turbines especially during periods of bad weather conditions.

Therefore, gearless approach is more preferable in the most cases, as gearbox breakdown

can be one of the common causes of the whole system failure and it requires a plenty of

maintenance. In addition, the gearbox and its own losses obviously affect the efficiency of

the whole system and causes unpleasant noise.

In (BAROUDI et al 2005) it is also stated that PMSG can be recommended alternative as

well even for newer smaller scale turbine design, since it allows better performance and

higher efficiency with smaller wind turbine blade diameter. More detailed discussions

about this promising concept of variable-speed WECS with PMSG and its comparison with

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conventional DFIG approach especially for large offshore wind farm applications can be

found in (LAMPOLA 2000) and (RAMTHARAN et al 2007).

1.1.1 Frequency converters in WECS

As described earlier, the contribution of power electronics is crucial for wind energy

conversion systems, as increasing share of wind in power generation will influence

significantly the dynamic behaviour of the power system. In addition, network operators

have to ensure that consumer power quality is not compromised. Hence, new technical

challenges emerge due to the increased wind power penetration, dynamic stability and

power quality, so it consequently implies new challenging requirements and demands for

power electronics converters (PECs) either.

The main aim of a PEC in any wind energy conversion system it has been developed for is

to integrate wind power with the electric grid. Moreover, power electronics system is used

to achieve variable speed operation while wind speed varies either. In addition, the use of

PECs for variable-speed operating WECSs allows enhancing its power extraction. In

variable-speed operation, a control method also designed to extract maximum power from

the wind turbine and provide desirable constant grid voltage and frequency, and this

controlling methods issue is discussed in Chapter 3 of this work.

Hence, full-power converters offer both variable speed operation of wind turbine and its

smooth integration to grid. In general, according to (NALLAVAN et al 2011) contribution

of modern semiconductor full-power PECs in WECSs can be summarized as follows:

Based on the wind speed, the generator speed is controlled by means of PEC, thus

variable speed operation is implemented, including gearless approach as well;

Enhancing of maximum power extraction from WTG;

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Constant power factor (PF) and as sinusoidal as possible output voltages and

currents are obtained, in order to supply quality power to the grid;

High level of reliability of the system, including both protection of the generating

unit and the grid;

The possibility of bi-directional power flow.

Thus, frequency converters can be determined as integral part of directly driven WECS

with PMSG. It should be also mentioned, that PECs for the modern trend of multi-

megawatt wind turbines for offshore applications should be able to provide higher voltage

and power capability. The possible topologies of available approaches for converters

utilized in WECSs are considered in the following chapter.

1.2 Converter topologies for high power applications.

The increase of the power capabilities of modern wind turbines in general, and wind

turbines with PMSGs in particular, definitely influence on requirements and appearance of

new power converter topologies capable to drive all desired power. In addition, the trend of

development higher voltage and current power semiconductor devices also still continues.

Thus, according to the latest generation of power semiconductor devices is capable to

support high-level voltages in the ranges up to 20kV (SUI 2007). However, such kind of

devices does not fully dominate even in high power application, due to utilization of variety

of topologies using medium power semiconductors. Further semiconductor devices used in

PECs of WECSs are considered in chapter 1.2.3.

The classification of modern available PEC topologies for high power applications is

presented in Figure 4.

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Figure 4. Classification of high-power converters. Adopted from (FRANQUELO et al 2008)

In general, among all represented converter topologies there are three the most interesting

ones from wind power generation point of view, they are two-level PWM converters,

matrix converters and multilevel (ML) converters.

The most conventional type of PEC for variable speed wind turbine (VSWT) widely

available in the current energy market is two-level PWM converter. It has relatively low

cost due to its maturity technology. Basic scheme of two-level converter is presented in

Figure 5, and it can be clearly seen two voltage source inverters (VSIs) on both generator

and grid sides divided by DC-link capacitor or just often called DC-link. In general, the

DC-link capacitor of a converter is an energy storage component of the system. In addition,

the capacitor of DC-link is the most vulnerable component of any indirect converter and it

significantly affects reliability of the system. In general, the capacitance of the intermediate

of the DC-link significantly influence on the performance of the VSI. Thus, it is reported in

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(PYRHONEN 2010), that generally DC-link capacitor is dimensioned in a way to be in a

range about 20 µF per one ampere of the rated value of the converter current.

Figure 5. Basic scheme of 2-level converter. Adopted from (KIM et al 2010).

There are some key drawbacks of 2-level converters which limit their application in

modern VSWT and yield to their displacement from the wind energy market by ML, in

particular 3-level converters. Among them can be noticed relatively high transients and

switching losses, oversized semiconductor components and poor quality of harmonic

content of output voltages and currents comparing with ML converters, which yields to

necessity of including complex and expensive filters (KIM et al 2010).

Another alternative approach is utilization of matrix converters, which have a key

difference from the both 2-level and ML converters in such a way, that the matrix converter

is capable of conversion of variable frequency AC of generator side directly into constant

AC frequency of the grid. Thus, passive DC-link capacitor is removed from such AC-AC

converter design, consequently more reliable performance and smaller dimensions of

converter system are obtained. However, the number of semiconductor switching devices is

also significantly increased for this topology.

As shown in Figure 6, the basic scheme for three-phase matrix converter connecting

generator unit with the grid consists of 9 semiconductor switches, which controlled in such

a way that any of three switches in one common leg cannot be turned on instantly. Then, to

provide bi-directional power flow total number of switches should be doubled up to 18.

Generator side: Rectifier DC-link Grid side: Inverter

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Clarified performance of matrix converters can be found in references (WHEELER et al

2002) and (JIA et al 2007).

Figure 6. Basic scheme of matrix converter (KIM et al 2010).

Despite certain advantages, some undesirable features still limit wide industrial use of

matrix converters. They can be reported as sensitivity to distortion in input power supply

and grid disturbances due to the lack of reactive component in the power circuit and rapid

change in the input voltage frequency when used in WECSs. In addition, the level of output

voltage is limited by certain level, and relatively high conduction losses should be

mentioned (KIM et al 2010).

The most promising PEC approach for modern VSWT is multilevel converters. Compared

with two-level converters, ML converters, which have various designs, comprise three or

more voltage levels. Such a design results in certain advantages. Firstly, lower total

harmonic distortion (THD) of output signals is obtained, compared with conventional 2-

level converters. It can be noticed as one of the key issue, due to increased share of wind

power contribution in total power generation. Secondly, multilevel converters are capable

for higher power capability, even using medium power semiconductor switches, due to

voltage sharing between levels, so ML converters are fully suitable for multi-megawatt

scale VSWTs. This results also in reduction of switching losses, since voltage values during

transients are also significantly decreased, as well as switching frequency can be increased

drastically compared with 2-level converters. In addition, one DC-link capacitor, is

replaced by two or more ones, which are also should be chosen during the design of the ML

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converter. However, as capacitors are the most expensive elements of the converter, the

number of semiconductor components and capacitors in ML converter yields to increased

costs for such applications (IKONEN et al 2005).

In general, for all ML converters the following formula for different possible converter

switching states is valid

Nsw=nm, (1)

where n is the number of voltage levels in the DC-link and m is the number of phases of the

converter. Thus, for three-phase two-level, three-level and five-level converters the variety

of different switching states is 8, 27 and 125, respectively.

Considering rectifier part of the ML converter, it should be mentioned that conventional

approach usually includes 6-pulse rectifier on the generator side. However, such an

approach cannot provide quality performance of full-power ML converter for the

application of PMSG in VSWT, which is in general scope of this thesis, due to the fact that

it cannot be fully controlled. The full-control converter implies the presence of controlled

both inverter and rectifier, which design is fairly demanding task. However, requirement of

full-controlled converter is crucial for modern multi-megawatt WTGs, in order to regulate

torque, rotational speed and power (MULJADI et al 1998).

In addition, unity power factor (PF) is required for modern high power rating VSWT, and

rectifier should be capable to provide it along with harmonic requirements of the grid.

Furthermore, regenerative capability and active mitigation of the system oscillations should

be provided. Therefore, it is crucial that the rectifier is an active part of the full-controlled

ML converter in order to provide harmonic mitigation and unity power factor for the whole

speed and load range (HAITHAM et al 2010).

Despite all mentioned above, multilevel converters are, however, still limited by drawbacks

of voltage unbalances, count of components and relatively complex modulation

approaches. In particular, a critical issue in three-level converters is the design of the DC-

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link capacitors, which already mentioned in previous discussion. Thus, special attention

should be paid to the unbalance in the voltage of the capacitors for the three-level

converters, which may cause a certain control problems (MELICIO et al 2010; KIM et al

2010).

Figure 7. a) Three-level FLC VSI; b) Three-level CHB VSI (POTASHKO 2011)

According to classification presented in Figure 4, except neutral point clamped (NPC)

converters there are also so called cascade half-bridge (CHB) and fly-capacitor (FLC)

multilevel converters available for high power applications, in particular for already

mentioned multi-megawatt WTGs. FLC voltage source converters (VSCs) are characterized

with twice higher switching losses than NPC converters with the same switching frequency,

in addition its design requires 5 capacitors comparing with 2 capacitors for the same 3-level

NPC design, so the cost of the system drastically increased. On the other hand, as it can be

seen from Figure 7 the total amount of semiconductor components is less than in NPC

application.

Another available approach CHB VSC is not in favour for this work due to its general

complicity and relatively high number of switching devices which results in increased

dimensions and high cost of the system. Furthermore, high switching losses are another con

of CHB VSCs. Therefore, the detail designs of CHB and FLC VSCs are outside the focus

of this thesis, however they can be found in the literatures (RUDERMAN et al 2009),

a) b)

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(HAITHAM et al 2010) and (MALINOWSKI et al 2010). Further, only scheme of 3-level

NPC inverter as a part of the converter is considered, which model and control strategy has

been discussed and implemented in the following chapters of the thesis.

1.2.1 Three-level Neutral Point Clamped inverter.

To build adequately performing simulation and control model of the NPC inverter the

principle of its design and performance should be fully clarified. So, the scheme description

according to Figure 8 follows and possible switching states are represented below.

In general, the circuit comprises three phases connected to the common DC-link capacitors.

The whole scheme consists of 12 active switches, isolated gate bipolar transistors (IGBTs)

in our case, with inversed power diodes connected in parallel and 6 neutral point clamp

diodes. Thus, switches S11, S21 and S31, either S14, S24 and S34 are called outer switches Sout,

as well as corresponding inverse diodes have the same indexes and also named Dout. All

three phases have the same structure and behaviour with assumption that load phases are

also equal and balanced, since further the first subscript number means the phase number is

replaced with ‘x’. However, it should be kept in mind that this assumption is valid only in

cases, when rough transients are not considered, as it is assumed during the simulations in

this thesis. Thus all the 6 remaining switches Sx2 and Sx3 and corresponding to them inverse

or free-wheeling diodes are named Sin and Din, respectively. The group of 6 diodes

connected to the neutral point further is marked as Dx5 and Dx6 or Dnpc.

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Figure 8. Three-phase three-level NPC inverter (BRUCKNER 2005).

As it was mentioned in previous chapter and according to (1) the number of possible

converter switching positions for three-phase 3-level inverter can be calculated as

Nsw=nm=3

3=27. (2)

All these switching positions correspond to the three possible states of each inverter phase

leg. Thus, independently of two other phases each phase terminal of the inverter can be

connected to DC bus in the three terminal points: upper positive ‘+VDC/2’ DC rail, neutral

‘0’ point or lower negative ‘-VDC/2’ DC rail. Thus, possible switching positions table of

three-level NPC inverter can be formed, as presented below.

Table 1. Switching positions for a phase of three-level NPC inverter.

State

Switch position

Sx1 Sx2 Sx3 Sx4

’+VDC/2’ 1 1 0 0

’0’ 0 1 1 0

’-VDC/2’ 0 0 1 1

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Then, consider the available current paths in each phase of the inverter both for positive and

negative phase currents formed by certain switch positions considered previously. From the

Figure 9 it can be clearly seen that all IGBTs and diodes might be stressed with maximum

levels of voltage and current Îph and VDC/2 respectively, and definitely these parameters

influence on the selection of the semiconductor devices for certain application

(BRUCKNER 2005).

Figure 9. Conduction paths for one phase of three-level NPC inverter (BRUCKNER 2005)

In principle, at any state of a phase two semiconductor devices provide a conduction path

for one direction. Thus, in case of upper path positive current flows through active IGBT

switches, whereas inverse diodes provide negative direction of current flow. Otherwise,

lower current path provide positive current flow through the power diodes, while negative

current flows through IGBTs there. It should be kept in mind that in NPC inverters active

IGBT switches, which are not utilized in forming corresponding path for current flow,

should be switched off, in order to prevent short-circuit failure. In contrast to ‘+’ and ‘-’

states, in zero state ‘0’ both upper and lower paths of neutral tap are utilized in order to

provide bi-directional current flow as it shown in Figure 9. So, in the NPC voltage source

inverter the utilization of the upper or lower NPC path is determined by itself with the

natural direction of the phase current (BRUCKNER et al 2005).

Thus a relatively simple theoretical operation principle allows to create easy implemented

control algorithm, especially thanks to symmetrical switching states for upper and lower

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halves of the NPC inverter topology. Since, generally control signals may be formed only

for the upper Sx1 and Sx2 switch branches. On the other hand such conduction paths created

by switching positions create uneven power loss distribution between switching devices.

More detailed discussion for both control and losses issues for NPC inverter are presented

in Chapters 2 and 3.

1.2.2 Three-level Active Neutral Point Clamped inverter

Bruckner (2001) first introduced the modified design of NPC converter, which is referred

as active neutral point clamped (ANPC) converter. This 3-level ANPC design was

developed in order to overcome the main drawback of conventional NPC approach, namely

the uneven loss distribution among the semiconductor devices, limiting output power of the

converter. This drawback has been eliminated with adding two active switching devices,

for instance IGBTs, in antiparallel with the clamping diodes. In general, such a modified

design provides additional current paths, but the total number of active switches is

increased up to 18, as it can be seen from topology of ANPC in Figure 10.

Figure 10. Three-phase three-level ANPC topology. Adopted from (BRUCKNER 2005)

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Consider any phase leg of the ANPC topology shown in Figure 10, in order to obtain

possible switching positions and states of the phase. Thus, additional active NPC switches

referred as Sx5 and Sx6 allow implement more than one state to connect the phase to the

neutral tap. These new zero switching positions form possible phase states ’0Up1’, ’0Up2’,

’0Low1’ and ’0Low2’ either positive ’+VDC/2’ and negative ’-VDC/2’, which are presented

in Table 2.

Table 2. Switching positions for a phase of three-level ANPC inverter.

State

Switches position

Sx1 Sx2 Sx3 Sx4 Sx5 Sx6

’+VDC/2’ 1 1 0 0 0 1

’0Up1’ 0 1 0 1 1 0

’0Up2’ 0 1 0 0 1 0

’0Low1’ 1 0 1 0 0 1

’0Low2’ 0 0 1 0 0 1

’-VDC/2’ 0 0 1 1 1 0

Comparing states of the NPC and ANPC inverters presented both in Table 1 and Table 2,

one can noticed that positive and negative states are similar for both topologies. The only

except is additional turned on switch Sx6 for ’+VDC/2’ state, which provides an equal

voltage sharing between Sx3 and Sx4. Similarly, the same function is provided by Sx5 for Sx1

and Sx2 in ’-VDC/2’ state. Thus, the voltage balancing is guaranteed across the inner

switches.

In contrast to NPC topology described in previous chapter neutral tap current paths of

ANPC topology are implemented with 4 states. Thus, if active NPC switches Sx2 and Sx5

are turned on ’0Up1’ and ’0Up2’ states are obtained, and the phase current is conducted

through the upper path of the neutral tap in both directions. Analogously, turned on Sx3 and

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Sx6 lower inner switches provide current conduction in both directions through the lower

path of the neutral tap in ’0Low1’ and ’0Low2’ sates. Obviously, all the four inner switches

Sx2, Sx5 and Sx3, Sx6 also can be turned on instantaneously, but this state is not considered

due to unclear current distribution among the devices (BRUCKNER et al 2005). In

addition, in case of upper NPC path is utilized IGBT Sx4 may be both turned on or off, as

well as Sx1 for lower neutral path. These additional switching alternatives can be utilized in

distribution of switching losses among the active switches. Thus, current paths

implemented by these four inverter neutral states as well as positive and negative paths for

the ANPC inverter are shown in Figure 11.

Figure 11. Possible conduction paths for one phase of three-level ANPC inverter. a) ’+VDC/2’ state;

b) ’0Up1’ and ’0Up2’ states; c) ’0Low1’ and ’0Low2’ states; d) ’-VDC/2’ state (BRUCKNER 2005).

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1.2.3 Switching devices of the inverter

In recent years, the field of high power applications has been one of the most actively

researched and developed area of power electronics, mainly due to increased power level

needs of industry and power generation. The development of new power semiconductor

devices obviously increases the power capability of medium voltage converters for high

power applications.

The development of high power converters started in the middle of 1980s with 4500V gate-

turn-off (GTO) thyristors introduced in commercial market. The GTOs dominated on the

market of high power applications until the end of 1990s, when insulated gate bipolar

transistors (IGBTs) and gate commutated thyristors (IGCTs) technologies were developed.

Nowadays these switching devices are mostly used in high power applications, including

multi megawatt VSWTs, due to its controllability, quality switching characteristics and

reduced power losses (RODRIGUEZ et al 2007).

Nowadays, Siemens, ABB and Converteam offer some three-level NPC inverters in range

of 2.3-6.5kV based on IGCT and IGBT modules technology. The selection of a certain

multi voltage inverter depends on a certain criteria. The most important are its initial and

operating cost, reliability, technical performance and power capability. The initial cost of

the inverter is largely influenced by the cost of the semiconductor devices due to its

contribution of about 40% of the total material cost of the NPC inverter. Operating cost is

mostly assesses with maintenance and efficiency of the inverter. Power capability and

corresponding dimensions are also important issues especially for WTG because of limited

space in windmills. The guideline for selection technique of appropriate application of 3-

level NPC converters can be found in (SAYAGO et al 2008).

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High voltage IGBT module is one of the most promising device technology nowadays,

which capable to provide standard voltage level ratings for high power applications, as it is

presented in Table 3 (SAYAGO et al 2008).

Table 3. Voltages of three-level NPC inverter available on the market.

Line-to-line voltage of

the system (DC-link

voltage)

Semiconductor device

voltage

2.3kV 3.3kV

3.3kV 4.5kV

4.16kV 6.5kV

However, it should be kept in mind that to achieve an output line-to-line voltage the

minimum DC-link voltage should be applied to switching device, calculated as follows

rmsLL,minDC, 2VV (3)

To determine the nominal DC-link voltage of the converter 4% f the theoretical value is

added in order to eliminate imperfections of a real system

minDC,nDC, 04.1 VV (4)

One of the feature of IGBT converters is that its modern technology is based on so called

power electronic building blocks (PEBBs), which include IGBT modules and have the

same interfaces and dimensions independently from their voltage levels (SAYAGO et al

2008). For instance, some parameters for the model of the inverter built during this work

have been taken directly from the datasheet of the 2.3kV IGBT module FZ1200R33KF2C

by Infineon, which can be found in Appendix 1.

The IGBTs are very popular in high power and high frequency applications, including

three-level NPC inverter simulated in this work. However, these applications require

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sophisticated thermal management systems to protect the utilized IGBTs and provide

reliable performance of the whole application system in general, as the devices commonly

operate with minimum safety margins due to the cost considerations (RAJAPAKSE et al.

2005).

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2 POWER LOSSES OF THE INVERTER

In general, power losses of any power electronic equipment comprise of power losses of all

components contained in the equipment. In electrical components the power losses caused

in the resistances of these components, so power losses, by nature, means heating of the

component. Such an undesirable in the most of applications heating limits the load

capabilities and affects either efficiency of the inverter or efficiency of the whole system. In

addition, if the temperature of any component of the system exceed a certain acceptable

limit due to untransfered heat or overload of the component, it could be finally damaged,

which in its turn might cause the failure of the whole system.

Conduction and switching losses of semiconductor devices occurred in three-level NPC

inverter during its performance are discussed in this chapter. In addition, along with loss

behaviour of the inverter, calculation methods used to assess amount of losses and its

implementation in the simulation model are also discussed here.

2.1 Commutations and losses in three-level NPC inverter

In general, switching and recovery losses are created during the commutation processes

between different switching states. The following discussion on commutations of NPC

converter is based on (BRUCKNER 2005). They are worth to mention it here since the

significant part of the thesis research is focused on losses occur during the inverter

performance. In the following discussion only on commutations obtained with positive

phase current direction are considered, however the resulting figures and tables for both

positive and negative currents are presented as well.

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As in previous chapter the commutation processes and losses occurred during them are

considered only for one ‘x’ phase of the inverter, as the principles are the same for all the

three phases. Firstly, consider the commutation from positive DC-rail, referred as ‘+’ state,

to neutral tap ‘0’ state, which initiated by turning off the outer switch Sx1, and results in the

current flow through the NPC diode Dx5. Then inner active switch Sx3 is also turned on,

however turn-on losses do not occur in it, because there is no current there during the

commutation. Instantaneously, Sx2 and Sx4 stay turned on and off, respectively. Thus, Sx1

and Dx5 devices are utilized in commutation, but only Sx1 experiences significant turn-off

losses, as turn-on losses of free-wheeling diodes are negligibly small and are not taken into

account during the further discussion and simulations as well.

Then, consider the reverse commutation from zero state’0’ to positive one ‘+’. It is initiated

by turning off Sx3, however turn-off losses are not experienced there, as case for positive

current is under observation. Following, after dead time Sx1 is turned on, since turn-on

losses occur in it, while Dx5 experiences recovery losses. Thus, both commutations are

presented in Figure 12, where Sx1 and Dx5 are encircled, as they experience switching losses

during these commutations for positive load current.

The commutations result switching losses in Dx1 and Sx3 at negative phase current also

shown in Figure 12. In this case the principles of losses behaviour in these devices are the

same as it was described for positive load current iph.

Figure 12. Commutations for both from ‘+’ to ‘0’ states and reversed. a) for positive load current b) for

negative load current. Adopted from (BRUCKNER 2005).

a) b)

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The commutation from zero state ‘0’ to negative state ‘–‘ and stressed switching devices

are shown in Figure 13. During the commutation four devices are employed. Thus, the

commutation is initiated by turning off the inner switch Sx2, immediately the current is

forced to Dx3 and Dx4. Then, Sx4 is turned on, while Sx3 is in on state. During these

transients only Sx2 experiences essential turn-off losses for positive current direction.

However, for negative load current this commutation yields significant turn-on losses in Sx4

and recovery losses in Dx6, as Sx3 stays in turn-on state during the commutation.

The back reversed commutation principle is based on turning off Sx4 firstly and turning on

Sx2 then. Thus, for positive load current Dx4 experiences recovery losses, while turn-on

losses in Sx2 occur. It should be noticed that although Dx3 connected in series with Dx4 also

turns off by nature, it does not face turn-off losses, due to Sx3 remains turned on and there is

no voltage across the Dx3 during the commutation, while the whole blocking voltage UDC/2

is adopted by Dx4 only. In case for negative load current turn-off losses occur in Sx4, as it is

turned off firstly. There no any losses are experienced by other devices for this

commutation in case of negative current direction.

Figure 13. Commutations for both from ‘0’ to ‘-’ states and reversed. a) for positive load current b) for

negative load current. Adopted from (BRUCKNER 2005).

As a result, switching losses distribution between all semiconductor devices is presented in

Table 3. It can be seen, that regardless up to four devices are utilized in each commutation,

a) b)

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only two or even one device experience essential switching losses during the commutation

(BRUCKNER 2005).

Table 4. Switching losses distribution between semiconductor devices for one phase in three-level NPC

inverter. - turn-on losses, - turn-off losses, - recovery losses.

Commutation Sx1 Sx2 Sx3 Sx4 Dx1 Dx2 Dx3 Dx4 Dx5 Dx6

Positive load current

From ‘+VDC/2’ to ‘0’

From ‘0’ to ‘-VDC/2’

From ‘-VDC/2’ to ‘0’

From ‘0’ to ‘+VDC/2’

Negative load current

From ‘+VDC/2’ to ‘0’

From ‘0’ to ‘-VDC/2’

From ‘-VDC/2’ to ‘0’

From ‘0’ to ‘+VDC/2’

Along with switching losses conduction losses are also experienced by semiconductor

devices during the inverter performance. The conduction losses distribution both for

positive and negative load current is presented in Table 4 according to NPC inverter

possible states.

Table 5. Conduction losses distribution between semiconductor devices for one phase in three-level

NPC inverter.

State Sx1 Sx2 Sx3 Sx4 Dx1 Dx2 Dx3 Dx4 Dx5 Dx6

Positive load current

‘+VDC/2’

‘0’

‘-VDC/2’

Negative load current

‘+VDC/2’

‘0’

‘-VDC/2’

Device

Device

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2.2 Commutations and losses in three-level ANPC inverter

The possible states for ANPC inverter have been considered in Chapter 1.2.2. The

commutations between these states and corresponding losses occur during the

commutations are considered in this chapter. In addition, to switching losses, distribution of

conduction losses in ANPC inverter is also presented below.

In contrast to NPC inverter, there are four alternatives for commutation from positive

‘+VDC/2’ state to neutral state in ANPC topology. Firstly, consider commutations to the

upper part of neutral tap. Thus, transient from ‘+VDC/2’ to ’0Up2’ initiated by turning off

Sx1 and then Sx5, while Sx6 has been already in off state. So, the inverter behaves in the

same manner as NPC during this commutation. Both commutations from ‘+VDC/2’ to

’0Up1’ and from ‘+VDC/2’ to ’0Up2’ are identical with only difference that in ’0Up1’ Sx4 is

turned on after Sx5. However, only Sx1 is stressed with positive load current during these

transients and experiences turn-off switching losses (RODRIGUEZ et al 2010).

The backward commutations from neutral tap to ‘+VDC/2’ positive state are implemented in

reversed order. Consequently, Sx5 is turned off first, then Sx1 is turned on, and Sx6 is turned

off finally for ’0Up1’, which yields in recovery losses in Dx5 and turn-on losses in Sx1 for

positive load current. The same commutations from ‘+VDC/2’ to ’0Up1’ and ’0Up2’ states

and reversed result in both switching losses in Sx5 and recovery losses in Dx1 for negative

load current. The all considered cases of commutations and corresponding lossy devices are

shown in Figure 14 (BRUCKNER et al 2005).

Commutations from negative state ‘-VDC/2’ to both ’0Up1’ and ’0Up2’ states of neutral tap

are similar, and losses occur during the transients in symmetrical devices are summarized

in Table 5.

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Figure 14. Commutations for both from ‘+VDC/2’ to ‘0Up1’ and ’0Up2’ states and reversed. a) for

positive load current b) for negative load current. Adopted from (BRUCKNER et al 2005).

In contrast to previous case commutation, during the transient from positive ‘+VDC/2’ to

zero ’0Low1’ state, the phase current iph commutates to the lower path of the neutral tap, as

it is depicted in Figure 15. During this commutation Sx2 is turned off first, then Sx3 is turned

on, while Sx1 and Sx6 switches stay in turn-on state, and switching losses do not occur there.

Thus, only Sx2 experiences essential turn-off losses for positive current direction. On the

other hand, for negative load current Sx3 and Dx2 are under stress and face to turn-on and

recovery losses, respectively.

The commutation in reversed direction from ’0Low1’ to ‘+VDC/2’ is analogous, but in

backward direction. Since, it is initiated by turning off the inner Sx3 switch, and Sx2 is turned

on after dead time. In this case, for positive load current, Sx2 experiences essential turn-on

losses, while recovery losses occur in Dx3 , due to blocking voltage after commutation. The

commutation with negative load current characterized only with essential turn-off losses in

Sx3 (BRUCKNER et al 2005). The description of these commutations both for negative and

positive load current is shown in Figure 15.

a) b)

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Figure 15. Commutations for both from ‘+VDC/2’ to ‘0Low1’ state and reversed. a) for positive load

current b) for negative load current. Adopted from (BRUCKNER 2005)

In general, both commutations from ‘+VDC/2’ to neutral states ’0Low1’ and ’0Low2’ result

in lower conduction path for both positive and negative load currents. However, during the

transient to ’0Low2’ neutral tap from positive DC rail Sx1 is turned off first, which yields in

turn-off losses in it, and Sx3 is turned on after that without any stress for positive load

current. On the other hand, turning on Sx3 during the commutation results in switching

losses both in Sx3 and Dx1 for negative load current.

The reversed commutation from zero ’0Low2’ to positive ‘+VDC/2’ state, during which Sx2

is turned on and Sx3 turned off, yields only in turn-on losses in Sx1 and recovery losses in

Dx3.Instanteneously, negative load current stressed Sx3 with significant turn-off switching

losses.

It should be mentioned, that losses distribution for commutations from both neutral states

’0Low1’ and ’0Low2’ to negative ‘-VDC/2’ state can be considered in the same manner.

Switching losses occur during these commutations in symmetrical devices of lower part of

ANPC topology are summarized in Table 5 , too.

b) a)

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Figure 16. Commutations for both from ‘+VDC/2’ to ‘0Low2’ state and reversed. a) for positive load

current b) for negative load current. Adopted from (BRUCKNER 2005).

According to Bruckner (2005) and Apeldoorn (2005), all the commutations of ANPC

inverter considered below can be divided in 3 types according to their switching losses

distribution and involved in commutation stressed devices.

Thus, first Type 1 comprises commutations, which involve one outer and one NPC device,

for instance commutation between ‘+VDC/2’ and ’0Up1’ or ’0Up2’ states for positive and

negative load currents with positive voltage polarity. During Type 2 commutations, there

are one outer and one inner devices experience switching losses. The example of Type 2

commutation can be switching between ‘+VDC/2’ and ‘0Low2’ states. Finally,

commutations of Type 3 involved in stressed switching two inner semiconductor devices

(BRUCKNER 2005).

The summarized classification of commutations and involved switching devices with

corresponding losses are presented in Table 5. All three types of commutations for positive

voltage and omitted negative one with respect to the both current directions can be found in

it.

a) b)

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Table 6. Switching losses distribution between semiconductor devices of one phase in three-level ANPC

inverter. - turn-on losses, - turn-off losses, - recovery losses

Commutation type Load

current Sx1 Sx2 Sx3 Sx4 Sx5 Sx6 Dx1 Dx2 Dx3 Dx4 Dx5 Dx6

1 From ‘+VDC/2’

to ‘0Up1’

+

-

1 From ‘0Up1’

to ‘+VDC/2’

+

-

1 From ‘+VDC/2’

to ‘0Up2’

+

-

1 From ‘0Up2’

to ‘+VDC/2’

+

-

3 From ‘+VDC/2’

to ’0Low1’

+

-

3 From ’0Low1’

to ‘+VDC/2’

+

-

2 From ‘+VDC/2’

to ’0Low2’

+

-

2 From ’0Low2’

to ‘+VDC/2’

+

-

3 From ‘0Up1’

to ‘-VDC/2’

+

-

3 From ‘-VDC/2’

to ‘0Up1’

+

-

2 From ‘0Up2’

to ‘-VDC/2’

+

-

2 From ‘-VDC/2’

to ‘0Up2’

+

-

1 From ’0Low1’

to ‘-VDC/2’

+

-

1 From ‘-VDC/2’

to ’0Low1

+

-

1 From ’0Low2’

to ‘-VDC/2’

+

-

1 From ‘-VDC/2’

to ’0Low2

+

-

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Using Table 5, appropriate commutations can be chosen, in order to distribute losses among

stressed devices by shifting switching losses from on device to another. However, in

practice, in order to achieve even loss distribution conduction losses also should be taken

into account. Thus, conduction losses distribution according to possible states of ANPC

inverter is summarized in Table 6 for both positive and negative load currents.

Table 7. Conduction losses distribution between semiconductor devices of one phase in three-level

ANPC inverter.

State

Sx1 Sx2 Sx3 Sx4 Sx5 Sx6 Dx1 Dx2 Dx3 Dx4 Dx5 Dx6

Positive load current

‘+VDC/2’

‘0Up1’

‘0Up2’

’0Low1’

’0Low2’

‘-VDC/2’

Negative load current

‘+VDC/2’

‘0Up1’

‘0Up2’

’0Low1’

’0Low2’

‘-VDC/2’

From Tables presented below both for NPC and ANPC topology one can see that

regardless the increased number of switching devices, the same number of IGBTs and

diodes experience both conduction and switching losses during the transients or staying in a

certain states. Thus in each state if three-level inverter four devices face to conduction

losses for both current directions, regardless the chosen NPC or ANPC topology.

Furthermore, the same commutation voltage VDC/2 and current iph stress the switches, as the

number of voltage levels remains the same. Therefore, it can be assumed that ANPC

Device

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topology can be used mostly for even distribution losses among the semiconductor devices

of the inverter, while the total inverter loss dissipation is not notably decreased.

Furthermore, based on the analysis of commutation, it can be clearly seen, that all the

commutations involve the same number of switching devices and make three of them (one

diode and two IGBTs) experience losses. Thus, all the commutations can be either assumed

as equal from total loss dissipation point of view (APELDOORN et al 2005).

2.2.1 Loss balancing in three-level ANPC converter

In practice, to achieve the most quality performance of ANPC converter loss-balancing

module is integrated to the control system of the converter. The modelling of this part of

the converter control is a demanding task, as it comprises different aspects of loss and

thermal behaviour of the converter. However, this system is crucial for reliable

performance of modern high power applications, including multi-megawatt VSWTs. On

the other hand, design of complex control systems including measurement equipment and

sensors also influences initial costs of the application.

In general, loss balance can be obtained only for each phase leg of the converter, as balance

between phases mostly depends on the load and grid properties. Thus, switching losses are

distributed in desirable way according with certain algorithm between switching devices of

topology by applying alternative types of commutations considered above. For instance, the

undesirable switching losses can be shifted from the overheated outer switches to the inner

ones, and then appropriate control vectors can be generated for ANPC to distribute losses

among inner devices as well (APELDOORN et al 2005).

In general, the main objective of the working algorithm of the loss-balancing system is to

optimize the control signal in order to keep the most stressed or hottest device of each

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phase as cool as possible (BRUCKNER et al 2005), for instance by choosing relevant

switching vector from available alternatives. Such a feedback-controlled balancing system

is shown in Figure 17.

Figure 17. Principle of the active loss-balancing system (BRUCKNER 2005).

As it can be seen from the block diagram, both switching and conduction losses are

calculated on-line from phase currents and DC-link voltages. In addition, junction

temperatures are calculated instantaneously. Then, using a thermal model of the converter

based, for instance on a Foster equivalent network, behaviour of the converter can be

simulated. Based on the obtained values of temperatures, losses and sampled phase currents

the most appropriate commutations paths are selected choosing certain suitable switching

positions, in order not to stress with significant losses the hottest semiconductor. Thus, the

loss balance requirements can be fulfilled (RODRIGUEZ et al 2010).

Thus, to achieve the quality loss balance of the converter several parameters and

characteristics of the system should be known during its performance, including real-time

parameters. Furthermore, aspects of heat network, junction temperatures of devices and, of

course, both switching and conduction losses are integral issues for such a system.

Therefore, the whole system requires efficient and modern embedded system to implement

its performance, on the other hand a certain assumptions can be made during the design in

order to simplify the approach and make it more feasible in practice.

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In this thesis, control of ANPC inverter has been implemented in the simplest case, with

assumption, that ambient temperature is constant. In addition, heat network as well as

model of thermal behaviour of the converter is out of the scope on this stage of modelling,

however it can be found in literature some approaches for implementation of the whole

system, as well as thermal behaviour issues, for instance in (MUSIKKA 2010) and

(HONSBERG et al 2009).

2.3 Power losses of semiconductor devices

Obviously, not only the fact of loss occasion, but the amount of power dissipation is crucial

in practice during modelling and design of the inverter. Regardless to the topology and type

of the switching device the generic nature of losses are analogous, and basic factors

influence the power dissipation in the same way.

Consider the principle switching characteristics of an ideal active switch shown in Figure

18. In general, the switch is turned on by applying positive control signal, for instance to

the gate of IGBT. Current through the switch start to increase after a delay time td during

rise time tr,i. Then, voltage across the switch falls during tf,v. These two intervals comprise

turn-on time duration

vf,ir,on ttt (3)

Analogously, after the delay time the turn-off transition occur in the reversed order during

turn-off time duration

if,vr,off ttt (4)

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Figure 18. Principle switching characteristics: a) control signals; b) switching waveforms; c) instantaneous

switch power loss. Adopted from (MOHAN et al 2003).

Thus, switching dissipation energy through the both transitions can be obtained by

estimating the areas under waveforms during the switching occasions

)(2/1 offoncondcomsw ttIVW (5)

Between turn-on and turn-off transitions the switch stay turned on. However, due to a

certain voltage drop occurs even during conducting through the switch, conduction energy

dissipation can be estimated as

condcondcondcond 2/1 tIVW (6)

a)

b)

c)

tr,i tf,v tr,v tf,i

ton

ton toff

Tsw=1/fsw

toff

Woff

Wcond

Won

Vcom Vcom

Vcond

Icond

I, V

W

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Dividing (5) and (6) by switching time period Tsw average switching and conduction power

loss values per switching period can be obtained

)(2/1)(2/1

offonswcondcom

sw

offoncondcomsw ttfIV

T

ttIVP

(7)

and

cond

condcondcond

2/1

T

IVP

(8)

From the obtained equations one can see, that switching power loss linearly depends on the

switching frequency. In addition, the proportion of the on-state period of the switch also

affects the conduction losses (MOHAN et al 2003).

In general, it can be concluded that, in principle, any switching losses calculation technique

is a geometrical method by nature. It should be kept in mind that linearized methods of

approximation and estimation of losses may be not accurate, as switching transient

waveforms usually have a complex shape, as it is shown in Figure 19. However, in practice

the accuracy of such methods is appropriate enough even with certain assumptions.

Thus, the aim of any calculation approach is to find as accurate approximation of

commutation current and voltage waveforms as possible. On the other hand it should be not

very complicated, as feasibility of the method is also important. There are certain methods

and approximation approaches can be found in literature, for instance in (RAJAPAKSE et

al 2005) and (FEIX et al 2009). The results obtained with geometrical representation of

current and voltage turn-on and turn-off waveforms are accurate enough, however, in

addition to detailed data-sheet data, some measurements should be also available.

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43

Figure 19. Real IGBT waveforms: a) turn-on b) turn-off. Adopted from (RAJAPAKSE et al 2005).

From the above discussion it can be summarized that power losses Ploss of any

semiconductor component comprise three following types: switching losses Psw,

conduction losses Pcond and blocking or leakage losses Pb (MOHAN et al 2003;

GRAOVAC et al 2009). However, normally blocking losses assumed to be neglected, thus

Ploss = Psw + Pcond + Pb ≈ Psw + Pcond. (9)

a)

b)

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2.3.1 IGBT and diode switching losses

Obviously, switching losses share a significant portion of the total amount of power losses

in a switching device. Since, accurate enough calculation of switching losses is an

important part of the loss-balancing system discussed previously. As it has been already

considered, due to derivative waveforms of commutation currents and voltages, linearized

loss model for calculation switching losses should be designed (RAJAPAKSE et al. 2005).

One of examples of such implementation can be found in (BIERHOFF et al 2004).

Recently, the equations for calculation switching losses occur in the components of two-

level application have been presented in (AARNIOVUORI et al 2012). However, the same

approach can be used for three-level inverter as well, since switching losses are calculated

for each independent device, regardless the topology and control method. Thus, the average

switching losses of an IGBT for the fundamental period fT in the three-level inverter can

be obtained as follows

swIGBT sw,

ratedrated

comcomIGBT sw, NE

UI

UIP (10)

Where swN is a number of switch changes during the fundamental period fT depending on

the fundamental frequency f =50 Hz

fT 1

f . (11)

However, it should be mentioned that any period under observation can be chosen.

Switching loss energy of the IGBT IGBT sw,E for the fixed datasheet parameters, including

reference commutation voltage and current, comprises turn-on and turn-off energies per

pulse, which are constant and can be taken from the datasheet

offonIGBT sw, EEE . (12)

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The actual commutation voltage comU corresponds to the DC-link voltage and depends on

the number of levels of the converter. Thus, for three-level inverter commutation voltage

comU is equal to the half of DC-link voltage

2DC

com

UU . (13)

In general, during the design the turn-on losses of modern fast recovery free-wheeling

diodes are not taken into account, due to its less than 1% share of the total switching losses

in the diode. However, the reverse recovery process during the transients produce

significant amount of losses, also referred as recovery losses of free-wheeling diode, which

obviously affect the amount of switching losses, as well as total losses in general

(RAJAPAKSE et al. 2005).

Analogously with IGBT switching losses, recovery losses for the free-wheeling diode can

be calculated

swrec

ratedrated

DCcom

rec2 NE

UI

UI

P (14)

where recE is reverse recovery energy taken from data-sheet for ϑ=125°C

2.3.2 IGBT and diode conduction losses

Obviously, along with switching losses conduction losses are also experienced by

semiconductor devices during the inverter performance. During the implementation of the

loss calculation model for the inverter the technique for conduction losses calculation in

IGBTs and diodes proposed in (GRAOVAC et al 2009) is utilized. Thus, conduction losses

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in IGBT or diode are calculated using common approximation of the semiconductor as a

series connected DC voltage source and a resistor. So, the voltage source represents IGBT

on-state zero-current collector-emitter voltage UCE0, while the resistor is a collector-emitter

on-state resistance of the IGBT RC

CCCE0CCE )( IRUIU . (15)

The parameters needed in calculation are taken from the data-sheet available in Appendix

1. It should be mentioned that the parameters of on-state resistance RC and threshold

voltage UCE0 are not given directly there, however sometimes these values can be given by

manufacturers in datasheets. Since, the determination technique of the threshold voltage of

the IGBT UCE0 and RC is represented in Figure 20. It can be also done by using any

software, for instance MatLab, thus more accurate margin can be obtained. It should be

kept in mind that obtained parameters correspond to the toughest conditions. In other

words, it is assumed that inverter performs at high ambient temperature or without cooling,

thus junction temperature of the device is ϑ=125°C, as it can be seen from the data-sheet.

Figure 20. Reading the UCE0 and RC using IGBT output characteristics from the data-sheet Appendix 1.

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Then, IGBT collector-emitter on-state resistance RC can be calculated as follows

C

CEC

dI

dUR . (16)

The instantaneous value of IGBT conduction losses is

)()()()()( 2

CCCCE0CCEIGBT cond, tIRtIUtItUtP , (17)

from which the average losses can be obtained by

2

RMSC,CavC,CE0

0

2

CCCCE0

cond0

IGBT cond,

cond

IGBT cond,

condscond

))()((1

)(1

IRIUdttIRtIUT

dttPT

P

TT

(18)

Where avC,I and RMSC,I are the average and root-mean-square value (RMS) IGBT currents

for the conduction period, respectively:

avC,I cond

0

C

cond

)(1

T

dttIT

, (19)

cond

0

2

C

cond

RMSC, )(1

T

dttIT

I . (20)

Analogously, the approximation discussed in the beginning of the chapter gives for the

anti-parallel diode the following

DDD0DD )( IRUIU . (21)

The diode parameters UD0 and RD are determined in the same way using typical transfer

characteristic taken from the data-sheet, as it is represented in Figure 21.

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Figure 21. Reading the UD0 and RD using IGBT transfer characteristics from the data-sheet Appendix 1.

In the same manner, the on-state resistance of the free-wheeling diode is obtained as

follows

D

DD

dI

dUR . (22)

The instantaneous value of the diode conduction losses is

)()()()()( 2

DDDD0DDD cond, tIRtIUtItUtP , (23)

from which the average losses of the diode for the conduction period can be obtained by

2

RMSD,DavD,D0

0

2

DDDD0

cond0

D cond,

cond

D cond,

condcond

))()((1

)(1

IRIUdttIRtIUT

dttPT

P

TT

(24)

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3 DYNAMIC SIMULATION AND MODULATION PRINCIPLES OF NPC AND

ANPC INVERTERS

Along with the converter topologies discussed in the previous chapter, chosen control

technique of a converter also impact on the efficiency and quality of the output voltages

and currents. There are some control strategies available to produce the desired output

signals, however pulse width modulation (PWM) is one of the most common used control

methods for power electronics converters (PEC) with alternating current output, due to its

maturity and known feasibility of implementation in embedded systems and

microcontrollers.

3.1 Modulation strategies for multilevel converters

From wind energy conversion system (WECS) point of view, the major objective of any

PWM method is to produce stable output voltage and current waveforms. However, another

essential aim of PWM schemes is to reduce the impact on the quality of the output signals,

for instance total harmonic distortion (THD), so they should comply with requirements of

the international standards.

In general, all the plenty of PWM methods despite of their different modifications are

usually categorized into three main groups. They are carrier-based PWM, selective

harmonic elimination (SHE) and space vector modulation (SVM) (KIM et al 2010). These

three PWM techniques are considered in the following discussion.

The most conventional PWM strategy is carrier-based PWM, due to relatively simple

implementation even using analog devices in the past. Nowadays digital implementation of

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this technique is also used, however the basic principle is the same for both

implementations, which is based on the comparison of the fundamental frequency

sinusoidal reference voltage with high frequency carrier signal. The switching states are

produced every time as reference signal intersects carrier signal. The basic control diagram

for three-phase pulse width modulator is presented in Figure 22. It should be mentioned,

that the frequency of the carrier signal corresponds to switching frequency of the inverter,

while reference signal frequency is equal to desired output voltage frequency.

Figure 22. Basic control diagram of three-phase carrier-based PWM.

In order to control multi-level (ML) inverters by based-carrier PWM some modifications of

this method can be employed. Thus, a modulation signal of level-shifted multilevel PWM is

represented in Figure 23. As it can be seen, the number of carrier signals for this multi-level

pulse width modulator is defined as (N-1), where N is the number of levels of the voltage

source inverter (VSI). Thus, for three-level NPC VSI N=2.

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Figure 23. Modulation signal for three-level application (RODRIGUEZ et al 2009).

The basic principle of SHE PWM strategy for three-level applications is based on the

control of the fundamental frequency by Fourier analysis of the inverter voltage, while the

most significant undesirable 5th

and 7th

harmonics are eliminated by using a certain

switching angles. This method from the control of three-level inverters point of view is a

suitable alternative, due to the fact that inverter can be operated at a relatively low

switching frequency. Since, the switching losses of semiconductor devices can be reduced

significantly. Thus, recently efficient SHE PWM technique has been presented for

multilevel converters, in particular for 3-level ANPC converter (PULIKANTI et al 2011).

Figure 24. SHE PWM modulation signal for 3-level ANPC application (PULIKANTI et al 2011).

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SHE approach is used quite widely in system level in distributed power generation systems,

for instance in large wind parks, in order to reduce the interconnection of harmonics and

eliminate the 11th

harmonic. There are obvious advantages of SHE PWM strategy usually

mentioned, such as high quality harmonic content of output voltage and reduction of

switching losses thanks to its harmonic elimination nature and low switching frequency

respectively. However, a certain drawbacks also exist, for instance relatively narrow

modulation range and complex implementation (BIERK et al 2009; PONTT et al 2003;

KIM et al 2010).

Another alternative to control three-level inverter is SVM method based on the space vector

theory with coordinate transformations. This method is the most widely utilized strategy for

three-phase NPC and ANPC three-level inverters. This fact can be explained with its

certain advantages, such as relatively simple digital implementation and quite wide linear

modulation range, as well as achievable low harmonic content of output signals and high

voltage capability (KIM et al 2010). Thus, this method has been implemented in this thesis

both for NPC and ANPC inverter topologies. So, more detailed discussion about SVM

technique to control NPC inverter is presented in the following chapter.

3.2 Space Vector Modulation of NPC inverter

As it is mentioned previously, in this thesis the mature and efficient SVM strategy is

offered to control three-phase NPC inverter in order to obtain desirable sinusoidal output

voltage. The output voltage waveform of each phase comprises three levels: 2/DCU , 0

and 2/DCU . In total, three-phase output sinusoidal voltages are generated by 33=27

switching combinations of the inverter, according to (2). The switching states of the

inverter have been already discussed in Chapter 1.2.1 and summarized in Table 1.

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The space vector diagram for the three-level inverter is presented in Figure 25. As the space

vector diagram of two-level inverter it is also regular hexagon consisting of six A, B, C, D,

E and F 60-degrees sectors. However, in contrast to two-level application each sector is

divided into four regions, which are equilateral triangles 1, 2, 3 and 4. As it also can be

seen from Figure 25 all the apices of the triangle regions correspond to 27 inverter

switching states: 24 active and 3 zero ones lying at the centre of the hexagon.

Figure 25. General representation of space-vector diagram of three-level inverter. Adopted from

(YAMANAKA et al 2002).

All the 27 switching states determine 27 base vectors, thus using these vectors output

voltage vector of the inverter Vref is formed. Each region as well as each sector contains

combination of relevant base vectors (switching states) utilized to obtain desired output

voltage vector. In addition, a certain sequence of switching positions which should be

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utilized for each region is also defined beforehand. So, a required sector is selected

according to the phase of the output vector, whereas region is identified with the amplitude

of the output vector.

The SV PWM strategy is based on the principle that the output voltage vector Vref can be

accurately enough calculated by using three adjacent vectors, also referred as the nearest

triangle vectors (NTVs) (KOCALMIS et al 2006; YAMANAKA et al 2002),

sref332211 TTTT VVVV (25)

where 1V , 2V and 3V are vectors defined by a triangle region where output voltage vector

Vref is located. The durations 1T , 2T and 3T for corresponding base voltage vectors

comprise the sampling time sT

s321 TTTT . (26)

Thus, the control SV PWM strategy for three-level NPC inverter has been implemented

with the algorithm based on two papers (KOCALMIS et al 2006) and (YAMANAKA et al

2002). The point of the designed algorithm includes four steps, as follows

1. Determination of the sector, in which desired output voltage vector Vref is located,

with according to phase of the vector.

2. Determination of the region, in which desired output voltage vector Vref is located,

with according to amplitude of the vector.

3. Definition of combination of switching positions (base vectors) utilized in forming

of Vref and sequence of its switching on in the combination.

4. Calculation of turning on durations for base vectors included in the combination.

The description of used methods and calculation approaches of each step are considered in

the following chapters.

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3.2.1. Determination of sector and region of SV

The first design step is determining the sector. Its determination is similar to two-level

applications, as phase angle α of the voltage vector is calculated and known, the sector,

where the reference output vector Vref is located, is determined based on the following

inequalities (KOCALMIS et al 2006)

If 0° ≤ α < 60°, then Vref is in sector A (27)

If 60° ≤ α < 120°, then Vref is in sector B (28)

If 120° ≤ α < 180°, then Vref is in sector C (29)

If 180° ≤ α < 240°, then Vref is in sector D (30)

If 240° ≤ α < 300°, then Vref is in sector E (31)

If 300° ≤ α < 360°, then Vref is in sector F (32)

Sector A for three-level inverter and its switching states are presented in Figure 26. It can

be seen, that every switching state of the inverter is described with combination of three

symbols corresponding to three phases of the inverter. Each symbol means connection of

corresponding phase to positive +UDC/2, negative -UDC/2 voltage and neutral point, ‘P’, ‘N’

and ‘0’, respectively. For instance, combination of N0P means that IGBT switches S11 and

S12, S22 and S23, S33 and S34 of the three-level NPC inverter topology in Figure 8 are turned

on.

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Figure 26. a) Sector A and its switching states; b) Space vector geometrical determination. Adopted

from (KOCALMIS et al 2006).

Determining the region in the sector is provided with projection of the vector Vref on the

borders of the sector, as it depicted in Figure 26. Thus, from Figure 26 (b) both m1 and m2

components can be calculated as follows (KOCALMIS et al 2006)

3

sin2

3

2

)3

sin(

n2

mbbam (33)

)3

sin(cos)

3cos()

3

sin2(cos n

nn1

mm

mm (34)

where modulation index mn corresponds to the length of the reference voltage vector Vref. In

general, the length of the maximum base voltage vector maxbase,V , for instance vectors a, b

m1

P0N

PNN P00

0NN

PPP

000

NNN

PP0

00N

A1

A3

A2

A4

PPN

m2

a)

b)

α

mn

m1

m2

mn

a

c

b

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and c from Figure 25, is equal to 2/3UDC. Thus, the maximum length for the amplitude of

the sinusoidal voltage is obtained as (PYRHÖNEN 2010)

maxbase,DCmaxbase,maxref,maxn, 866.0)3/1(2/3 VVV Um (35)

Thus, modulation index is

0 < mn ≤ 0.866. (36)

Therefore, the following inequalities are used to determine the region.

If m1 ≤ 0.5, m2 ≤ 0.5 and m1 + m2 ≤ 0.5, then Vref is located in Region 1 (37)

If m1 > 0.5, then Vref is located in Region 2 (38)

If m1 ≤ 0.5, m2 ≤ 0.5 and m1 + m2 > 0.5, then Vref is located in Region 3 (39)

If m2 > 0.5, then Vref is located in Region 4 (40)

3.2.2 Determination of switching states and their sequences

In general, transitions between switching states inside the regions are provided according to

the criterion of minimum switching changes. Since, for the constant modulation index only

one phase of the inverter changes its switching state, while other two phases remain in the

same state during a commutation, as it can be seen from space vector diagram in Figure 25.

In addition, for the following discussed sequences changing a state of any phase provided

by switch changes of two active switching devices of the inverter model.

Thanks to the symmetry of upper and lower parts of NPC inverter topology, vector of

control signals only for upper part is formed directly, whereas control vector for the lower

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part is generated just by inversing the binary code containing in the vector control. Thus,

the switching change of only one IGBT at any transition is considered, while corresponding

second IGBT is switched automatically due to control implementation approach.

The directions of switching sequences in the regions for all sectors are shown in Figure 27.

For instance, the switching orders for four regions and corresponding phases states of

sector A are as follows, according to Figures 25 and 27 (YAMANAKA et al 2002):

For region A1, as the switching direction is clockwise: PPP, PP0, P00, 000, 00N, 0NN,

NNN.

For region A2, as the switching direction is clockwise: P00, P0N, PNN, 0NN.

For region A3, as the switching direction is counter clockwise: PP0, P00, P0N, 00N.

For region A4, as the switching direction is clockwise: PP0, PPN, P0N, 00N.

Figure 27. Vector diagram for three-level inverter with directions of switching sequences.

Sector B

Sector C Sector A

Sector D Sector F

Sector E

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Then, consider two conventional alternatives for forming sequences of switching states of

the inverter. Both symmetrical and asymmetrical orders for region A2 are shown in Figure

28.

Figure 28. The asymmetrical (a) and symmetrical (b) switching sequences for sampling period Ts. Adopted

from (YAMANAKA et al 2002).

As it can be seen from Figure 28, the symmetrical approach requires twice more switching

transitions per one sampling period Ts, than asymmetrical one does. However, for both

sequences the following expression is true

sTttt 321 (41)

P P P 0 0 P P P

0 0 N N N N 0 0

0 N N N N N N 0

A2 V

U

W

A2 V

U

W

Ts Ts

Ts

t1/2 t2 t3 t1/2

t1/4 t2/2 t3/2 t1/4 t1/4 t2/2 t3/2 t1/4

a)

P P P 0 0 P P P

0 0 N N N N 0 0

0 N N N N N N 0

b)

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where t1, t2 and t3 are duration times of applying corresponding NTVs. The calculations of

these durations for each region are discussed in the following chapter. In addition, for three-

level inverter, as well as for two-level one, the sampling time can be calculated as

kfTs

6

1 (42)

where k is a total number of base vectors formed in one sector, and f is the fundamental

frequency. In this thesis, as inverter is a grid side application of the frequency converter, f =

50 Hz is the grid frequency.

In general, the appropriate switching sequence approach is chosen based on certain

compromise between better quality of output signals on one hand and reduced switching

losses of the IGBTs and more simple implementation on the other one. Thus, symmetrical

approach provides better harmonic content of output voltages and currents, due to twice

more switching transitions, however the control of the inverter becomes either more

awkward, especially during modelling, as it is described in Chapter 4.1. In addition,

complex and sophisticated analysis of the quality of output signals is out of the scope in

this thesis. However, general harmonic content analysis of output signals have been

provided during the simulations and THD has been evaluated as well. The obtained results

are also presented in Chapter 4.

Thus, the asymmetrical switching sequences have been chosen and utilized in the

simulation model, due to its more feasible implementation and reduced switching loss

dissipation. The pulse patterns and switching states for three phases in four regions of

sector 1 are presented in the diagram shown in Figure 29.

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Figure 29. The asymmetrical switching sequences for one sampling period Ts in regions A1-A4.

Adopted from (YAMANAKA et al 2002).

t1/4 t3/2 t2/2 t1/2 t3/2 t2/2 t1/4

t1/2 t2 t3 t1/2

t2/2 t1/2 t3 t2/2 t1/2

A2 V

U

W

A3 V

U

W

A1 V

U

W

W

A4 V

U

W

0 N N N N N N 0

P P P 0 0 P P P

0 0 N N N N 0 0

P P P 0 0 0 N N 0 0 0 P P P

P P 0 0 0 N N N N 0 0 0 P P

P 0 0 0 N N N N N N 0 0 0 P

P P P 0 0 0 0 P P P

P 0 0 0 N N 0 0 0 P

P P P 0 0 0 0 P P P

P P P 0 0 P P P

P P 0 0 0 0 P P

0 N N N N N N 0 t1/2 t3 t2 t1/2

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Therefore, as it can be seen from the diagram below, during sampling period Ts there are 7

and 5 switching changes in the first and third regions respectively. Both second and fourth

regions are characterized with 4 switching transients per region. The time periods during

which the corresponding to each region NTVs utilized are also shown under each region

pattern in Figure 29. These durations t1, t2 and t3 of applied NTVs for all the regions are

calculated in the following chapter.

3.2.3 Calculating the switching times and durations

As it has been already considered, the asymmetric switching sequences have been

implemented in the simulation model. However, for changing the switching combination

from asymmetric to symmetric one, all the time durations should be just divided by two. In

addition, the calculations of the time durations t1, t2 and t3 are independent from the sector,

in which the desired output voltage vector Vref is located. Thus, regardless to the number of

sector the phase angle α of Vref is chosen for calculations from the range

0° ≤ α ≤ 60°. (43)

In general, durations t1, t2 and t3 can be defined as weighting coefficients calculated from

geometrical representations of applied NTVs. The time lengths for the utilized in the

simulations NTVs are calculated according to formulas taken from (YAMANAKA et al

2002).

Thus, for first regions durations are calculated

))3/sin(21(1 ns mTt (44)

)3/sin(22 snTmt (45)

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sin23 snTmt (46)

In second regions base vectors are applied with the following durations

))3/sin(1(21 ns mTt (47)

sin22 snTmt (48)

)1)3/sin(2(3 ns mTt (49)

Base vectors of the third regions for all sectors are characterized with

)sin21(1 ns mTt (50)

))3/sin(21(2 ns mTt (51)

)1)3/sin(2(3 ns mTt (52)

Finally, durations of applying base vectors in the fourth regions are

))3/sin(1(21 ns mTt (53)

)3/sin(22 snTmt (54)

)1sin2(3 ns mTt (55)

For all time durations the expression for sampling time Ts (40) is fair. However, for these

calculations modulation index nm is always taken equal to unity during the simulations.

Thus, NTV duty-cycle calculations for all regions can be summarized in Table 7

(YAMANAKA et al 2002).

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Table 8. Time durations of adjacent NTVs utilized in SVM control model.

Region Applied NTVs Time length of NTV applying

A1, B1,

C1, D1,

E1, F1

op, oo, on ))3/sin(21(1 ns mTt

ap, an )3/sin(22 snTmt

bp, bn sin23 snTmt

A2, B2,

C2, D2,

E2, F2

ap, an ))3/sin(1(21 ns mTt

c sin22 snTmt

a )1)3/sin(2(3 ns mTt

A3, B3,

C3, D3,

E3, F3

ap, an )sin21(1 ns mTt

bp, bn ))3/sin(21(2 ns mTt

c )1)3/sin(2(3 ns mTt

A4, B4,

C4, D4,

E4, F4

bp, bn ))3/sin(1(21 ns mTt

c )3/sin(22 snTmt

b )1sin2(3 ns mTt

The NTVs and regions are referred according to the vector diagram and pulse patterns

diagram shown in Figure 25 and Figure 29, respectively. For instance, it can be seen that

total time length for base vectors op, oo and on is 1t . However, the total length 1t for these

vectors is divided in the following proportions for the first regions: t1/4 for op-vector, t1/2

for oo-vector and t1/4 for on-vector. Analogously, 2t and 3t are divided between ap, an and

bp, bn base vectors with certain proportions, thus the whole switching period Ts comprised

from 7 durations for A1, B1, C1, D1, E1 and F1 regions. The duty-cycles for all remain

regions are divided in the same manner according to the patterns in Figure 29.

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4 SIMULATION METHODS AND RESULTS

In this chapter, modelling and simulation of both NPC and ANPC three-level inverters have

been performed with RL-load using MatLab/Simulink package program. In addition, based

on the discussion in Chapter 2 losses calculation model is performed, too.

4.1 Modelling of three-level inverter controlled with SVM

The simulation model of three-level NPC inverter has been built in MatLab/Simulink

package program. The general models of the inverters with control block and loss

calculation module is presented in Appendix 2. The control algorithm of SVM technique

has been implemented with asymmetric sequences of inverter states and forming six base

vectors of output voltage in each sector. The frequency of output voltage is assumed to be

constant (50 Hz).

In convenience, the control model can be divided in 4 functional blocks shown in Appendix

3. The first one is ‘Definition_of_sector_and_angle’, where the frequency and amplitude of

output voltage is defined. The second block ‘Definition_of_Region’ is used to specify the

region location of the reference output voltage vector Vref. The block

‘Conducting_Time_Calculator’ is based on equations (43) - (54), where time durations of

applying base vectors are calculated for each region. Finally, ‘Switching_Control’ is the

block of logic elements and multiple switches perform connection, shift and switching of

base switching states of the inverter. Obviously, the last block differs in certain extent for

NPC and ANPC models, however its basic principle is the same for both models.

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4.1.1 SVM control of NPC inverter model

The input signals for SVM control block are the modulation index m and frequency f of

output signal. The block ‘Definition_of_sector_and_angle’ is shown in Appendix 4. The

sequence of sector number is defined with digital counter, and the period of changing the

sector number is

6secsT

T (56)

In addition, the amount of forming base vectors in the sector is also defined here with

sequence of the phase angle α, in particular the sequence discretely varies from 0° to 50°

with 10° step. The discrete change of α is initiated by every pulse of digital pulse generator.

The period of discretization is defined as

6s

d

TT (57)

Thus, control signals for six base vectors are formed for each sector. The outputs of the

‘Definition_of_sector_and_angle’ block are phase angle in range from 0° to 50° and

number of sector from 1 to 6.

Figure 30. The variation of phase angle α during fundamental period.

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The variation of phase angle α is shown in Figure 30. It can be also seen that during one

fundamental period Tf=0.02 the angle is counted six times up to 50 degrees, which

corresponds to 6 sectors. The counter of the sector number is reset every fundamental

period, thus output of the counter is control signal containing the number for enabling one

of six sectors.

The content of ‘Definition_of_Region’ block is presented in Appendix 5. Here, the

calculation is performed according with (36) - (39). As a result, the region, where the

output voltage vector is located, is defined. The inputs of the block are varying phase angle

α and modulation index m. The synchronization of calculations is performed with standard

Triggered Subsystem.

The outputs of the block are four digital control signals, which define the location of output

voltage vector. Thus, at any time the base vectors for only one region should be applied,

since the only one output signal contains positive control voltage, whereas the three others

are zero. For instance, the signals for regions are shown in Figure 31. As it can be seen for

modulation index m=1, the output vector is located in 2 and 4 regions.

Figure 30. The signals defining regions 1, 2, 3 and 4 for m=1.

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The calculation block for time durations t1, t2 and t3 of applied base vectors can be found in

Appendix 6. The calculations in ‘Conducting_Time_Calculator’ block are based on (43) -

(54) for each region. There are three inputs for this block, they are sampling time Ts,

modulation index m=1 and varying phase angle α. The output signals are durations of

applying vectors for four regions, which are identical for all sectors, so there are twelve

output signals, according to Table 7.

Then, the signals of time durations t1, t2 and t3 from ‘Conducting_Time_Calculator’ block

are one of the inputs for ‘Switching_Control’ compound module consisting of several

blocks, as it shown in Appendix 7. In general, the block contains four control channels for

four regions and the twelve time duration inputs, thus three t1, t2 and t3 time durations are

connected to each region block. In addition, the signals defining the region and sector are

the other two inputs.

The forming of asymmetric sequences of pulses with desirable durations as it depicted in

Figure 29 is provided in internal blocks ‘Switching_Sequence’. The principle of performing

for each block is similar, but the only difference is the number of switching changes and

lengths of forming pulses for each region. Therefore, the following method of

implementation is considered only for one region, for instance for region 2.

For region 2 the asymmetric sequence of switching states is formed in

‘Switching_Sequence2’ internal block, and it can be written as 22

132

1 ttt

t .

Thus, the inputs for this block are the signal defining the region 2, the signals of time

durations t1/2, t2 and t3 calculated for vectors formed in region 2 and synchronizing pulses

utilized to initiate the forming of sequences. The signals defining the length of pulses are

compared with reference signal from digital counter and using the logic elements desired

sequence 22

132

1 ttt

t is obtained, as it shown in Figure 31.

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Figure 31. The sequence of pulses region. theof signal control and2

1t

3t2t2

1t

Analogously, the following sequences4222224

1231321 ttttttt ,

and 2222

123

12 ttt

tt blocksin formed are

221

231 t

ttt

for

regions 1, 3 and 4, respectively.

Then, formed sequences of pulses are distributed between inputs of IGBTs of the inverter

simulation model according with the vector diagram shown in Figure 25 above. In addition,

the distribution of base states of the inverter is also provided here with respect to the sector,

which is defined with the signal coming from ‘Definition_of_sector_and_angle’ block. In

the model, multiple switches are utilized in order to obtain appropriate inverter states.

There are four multiple switches with six alternative base vectors formed in region 2 for all

six sectors in the block corresponding to region 2. Obviously, the number of the switches is

equal to the number of time pulses, thus for region 2 sequence 22

132

1 ttt

t

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there are four multiple switches with six stored base vectors corresponding to every time

length of the sequence. Thus, there are seven, five and four multiple switches for 1, 3 and 4

regions, containing six base vectors for every sector of the diagram.

The variation of the signal from 1 to 6 defines the number of the sector, thus reading of

appropriate base vector from the switch is initiated. Each base vector of the switch contains

6-bit binary code defining a desirable combination of turned on 6 IGBTs of upper half of

the NPC inverter. As it has been mentioned previously, the upper half IGBTs Sx1 and Sx2

perform in antiphase with lower half ones Sx3 and Sx4 respectively of the NPC inverter.

Since, control signals contains six-digit vectors for upper part of three-phase inverter,

whereas control signals for the lower part are obtained just with block of logical inversion.

In addition, the block ‘Switching_Control’ contains compound logical subsystems, which

provide applying the combination of desired switching positions for the period of time,

corresponding, for instance to t1/2, t2 and t3 time durations in region 2. Then, control pulses

corresponding to a certain switch are summed up with operator of logical addition OR with

four inputs, corresponding to four switching states in region 2 for four time durations,

discussed above. Further, the control pulses are serially multiplied with the signal of

corresponding region in blocks of logical conjunctions. Finally, obtained control pulses for

every one IGBT analogously summed up with OR-operators, thus control signal with

desired duration for every switch is obtained for a certain moment of time.

The only difference in control models of SVM for NPC and ANPC inverter is the

implementation of forming the base switching states of the inverter. Thus,

‘Switching_Control’ block is more complicated for ANPC application, due to the fact that

control vector for the ANPC inverter is not symmetric, as upper and lower parts in the

ANPC inverter do not perform in opposite phase, and specific switching combinations

should be applied, as it was presented in Table 2. Thus, in general asymmetric control

vector for ANPC inverter contains 18-bit code for all switches instantaneously for three

phase legs of the inverter.

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The power electronics part of the simulation model with measurement model to assess

losses has been built from IGBTs, wheel-forward diodes and measurement elements of

SimPower library of Simulink. The both NPC and ANPC inverter models are presented in

Appendix 8.

4.2 Simulation results for NPC and ANPC inverters

The first step of modelling is the simulation of NPC and ANPC inverters for RL-load.

During the simulations DC-link voltage and output frequency are assumed to be constant

and modulation index m=1. Thus, basically regions 2 and 4 are utilized during the

simulations, however for NPC inverter the model is capable to perform in all the four

regions and full modulation index range, except overmodulation mode, when m>1. The

IGBTs and diodes parameters for the inverter are taken from the data-sheet Appendix 1 and

obtained from Figures 20 and 21.

Table 9. Inverters and loss calculation model simulation parameters.

Parameter Explanation Value

UDC DC-link voltage [kV] 2.8

Rload Load resistance [Ω] 1

Lload Load inductance [mH] 2

ttol The minimum pulse length [µs] 50

tr Rise time [µs] 0.2

tf Fall time [µs] 0.2

fsw Switching frequency [kHz] 1.8

UCE0 Threshold voltage of IGBT [V] 1.9

RC IGBT collector-emitter on-state resistance [mΩ] 2

UD0 Threshold voltage of free-wheeling diode [V] 1.4

RD On-state resistance of free-wheeling diode [mΩ] 2.3

Eon Turn-on energy loss per pulse [mWs] 2200

Eoff Turn-off energy loss per pulse [mWs] 1550

Erec Free-wheeling diode reverse recovery energy [mWs] 1550

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In general, the given values correspond to the toughest conditions, when junction

temperature of devices is ϑ=125°C. Simulation results shown in Figure 32 and Figure 33

are obtained for output frequency f=50Hz and modulation index m=1. Obviously, obtained

results are generally identical for NPC and ANPC inverters, as the same modulation

strategy with the equal parameters is utilized during the simulations. Thus, Figure 32

illustrates output line-to-line voltage waveform with five levels.

Figure 32. The line-to-line output voltage waveform for f=50Hz and m=1.

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Figure 33. Three-phase output current waveforms and its spectrum for f=50Hz and m=0.866.

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Table 10. Comparison of obtained values of harmonic currents and permitted values from IEC 61000-

4-7 standard.

Harmonic

order

Permitted value of related harmonic

currents according to IEC 61000-4-7

for 10kV networks

Obtained values of harmonic

currents for ANPC inverter model

5 0.058 0.0255

7 0.082 0.0157

11 0.052 0.0078

13 0.038 0.003

17 0.022 0.0035

19 0.018 0.0046

23 0.012 0.0048

25 0.010 0.0106

In general, considering obtained waveforms of voltages and currents the quality of

performance of the inverter model can be assessed.

For instance, the output current harmonic content obtained with Simulink FFT-analysis is

presented in Figure 33 and Table 9. From its spectra it can be clearly seen the fundamental

50 Hz first harmonic, and THD is equal to 3.49% for ANPC inverter. During the

simulations, the tolerance parameter for minimum pulse length has been varied in narrow

ranges, however the THD value for both NPC and ANPC models do not exceed 3.5% for

these simulations.

The quality of output signals can be increased with implementation of symmetrical

switching sequences instead of asymmetrical ones, which are discussed in Chapter 3.2.2.

Thus, the number of switching transitions can be twice increased in order to reduce current

ripple. On the other hand, it can lead to significant increase of the switching losses and

overheating the components of the inverter. Therefore, as an option a simple LCL-filter can

be designed for the grid side to improve harmonic content of output signals.

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4.2.1 Comparison of losses calculation results and efficiency

Then, losses calculation results are considered. The results were obtained according to the

description of the methodology from Chapter 2.3.1 and 2.3.2. It should be noted that the

following assumptions were adopted to calculate power losses of the devices during the

simulations. Firstly, the load current is assumed to be sinusoidal and current and voltage

ripples are also neglected. Secondly, the dead times of switching devices are not taken into

account during the calculation (FLORICAU et al 2009). In addition, DC-link voltage is

kept constant and auxiliary losses corresponding to stray inductances in the inverter are also

neglected, and almost unity power factor (PF) is also assumed. Moreover, due to specific

modulator model m=0.866 is kept during the simulations. Thus, the total power dissipation

of the inverter is calculated as the sum of total conduction and switching losses.

The following Tables 11 and 12 show the distribution of conduction and switching losses

between devices for a phase for the toughest conditions.

Table 11. Losses distribution between devices in NPC inverter model.

Device Sx1 Dx1 Sx2 Dx2 Sx3 Dx3 Sx4 Dx4 Dx5 Dx6

Conduction

losses [W] 1290 19 1538 19 1538 19 1290 19 279 279

Switching

losses [W] 365 10 6 10 6 12 355 12 138 142

Total

losses [W] 1655 29 1544 29 1544 31 1645 31 417 421

Conditions: Eupec 3.3kV IGBTs Appendix 1 for ϑ=125°C, UDC=2.8kV, Iph=1.2kA,

fsw=1.8kHz, m=0.866, PF≈1

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Table 12. Losses distribution between devices in ANPC inverter model.

Device Sx1 Dx1 Sx2 Dx2 Sx3 Dx3 Sx4 Dx4 Sx5 Dx5 Sx6 Dx6

Conduction

losses [W] 1308 15 1343 93 1342 93 1308 15 174 207 173 207

Switching

losses [W] 140 13 112 87 111 88 140 14 105 65 104 63

Total

losses [W] 1448 28 1455 180 1453 181 1448 29 279 272 277 270

Conditions: Eupec 3.3kV IGBTs Appendix 1 for ϑ=125°C, UDC=2.8kV, Iph=1.2kA,

fsw=1.8kHz, m=0.866, PF≈1.

In general, as it is known, due to the symmetrical structures of NPC and ANPC topologies,

the loss behaviour of the upper and lower half components is similar for the both inverters.

Therefore, the symmetrical switches Sx1 and Sx4 are stressed equally, as well as Sx2 and Sx3.

In addition, simultaneously conducting Dx1 and Dx2 as well as Dx3 and Dx4 for NPC inverter

are also stressed equally. Actually, for PF is close to unity, there should be no losses for

FWDs, however small inductance in the load cause conducting losses there as well. The

current waveforms for the corresponding semiconductors can be found in Appendix 10.

The approach of losses distribution between outer and inner devices using the similar SVM

technique has been implemented for ANPC inverter. As it can be seen, the symmetrical

behaviour of ANPC topology also yields in equal losses for outer and inner

semiconductors.

As it can be seen from the both tables above the total losses distributed more evenly

between switching devices, due to increased number of active switches up to 18 and created

alternative current paths in the middle NPC part of the topology. Thus, outer symmetrical

switches Sx1 and Sx4 of ANPC topology are less stressed with total losses, comparing with

NPC one. In addition, Table 11 shows that NPC components are significantly stressed due

to the lack of alternative paths for both negative and positive load current during all the

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operation cycle, as it has already discussed in theory in Chapter 1.2.1. Therefore, additional

active switches in NPC point of ANPC inverter share the losses creating alternative ways

for current flow, since the inner and NPC semiconductors are unloaded to certain extent in

ANPC application.

For the same simulation conditions, the following total power loss calculation results are

presented in Table 12 for NPC and ANPC models.

Table 13. General loss distribution and efficiency of NPC and ANPC inverter models.

Loss type NPC ANPC

IGBTs conduction losses [kW] 16.95 16.95

Diodes conduction losses [kW] 1.89 1.89

Total conduction losses [kW] 18.84 18.84

IGBTs switching losses[kW] 2.2 2.14

Diodes switching losses[kW] 0.97 0.98

Total switching losses[kW] 3.17 3.12

Total loss dissipation [kW] 22.01 21.96

Efficiency, % 98 98

Conditions: Eupec 3.3kV IGBT-module from Appendix 1 for ϑ=125°C, UDC=2.8kV,

Iph=1.2kA, fsw=1.8kHz, m=0.866, PF≈1.

The obtained results show that conduction losses share significant part of total losses for

both topologies, and the most stressed devices are active IGBT switches, whereas

conduction and switching losses of free-wheeling diodes share less of total loss dissipation

for chosen simulation conditions. Furthermore, the conduction losses are equal, as the one

direction current flow is always provided by two components for both topologies. The

switching losses are mostly affected by utilized PWM method and switching frequency,

however the difference in their values between inverters is not significant either. In

addition, the total loss dissipations are approximately the same for NPC and ANPC

inverters, so, as it has been already mentioned previously, the aim of implementation of the

Simulation model

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ANPC is not to save total inverter losses, but distribute them evenly between the

components.

It should be mentioned that obtained results can be affected by some reasons, for instance

rough approximations and assumptions during the modelling and calculations. In addition,

the system with ANPC model is simulated with just ordinal sequences of NPC base

alternative vectors, whereas quite fair results can be obtained only with integration of

thermal behaviour of the inverter.

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5 SUMMARY AND CONCLUSIONS

As a contribution to previous studies in this thesis the SVM technique to control NPC and

ANPC inverters has been implemented in Matlab/Simulink environment. In addition, the

obtained simulation models have been utilized to investigate the distribution of both

switching and conduction losses between the components of the inverters. The analysis also

includes the calculation of total loss dissipations and efficiencies for both NPC and ANPC

inverters.

During the implementation of ANPC modelling an unequal distribution of power losses of

three-level NPC inverter has been overcome. The improved ANPC inverter model has been

simulated, and, as a result obtained waveforms of output voltages and currents show the

quality performance of the inverter. Thus, harmonic content of output signals correspond to

IEC 61000-4-7 international EMC energy supply quality standard and THD does not

exceed the accepted values. However, a simple model of grid filter can be implemented in

order to improve the model or make it more realistic, as real power converters are usually

include a certain filters in order to protect both the grid from the converter and vice versa.

The methods of calculations has been utilized in simulations are commonly used in

practise, however the assumptions which were accepted during the simulations may

essentially affect the obtained results. In general, obtained results correspond to the

theoretical issues discussed in background theories of the thesis and the similar results can

be found in and (FLORICAU et al 2009). Thus, the most stressed devices of NPC

application have been revealed. Then, extended topology of ANPC has been simulated, in

order to achieve more even distribution between semiconductors, so the losses distribution

and total loss dissipation for the both topologies can be compared. However, it should be

kept in mind that without relevant thermal behaviour model of the inverters the simulations

could be incomplete.

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Thus, the conduction and switching losses have been calculated for each component of

NPC and ANPC structures. Then, the relations and distribution between conduction and

switching losses among the semiconductors have been also investigated. Also, it has been

shown that the total losses are the same for both structures.

In general, designed models can be characterized as base ones and not flexible enough,

which can be used for different simulations by adding desired modules into them. For

instance, more complex analysis with varying PF values and sophisticated control strategies

can be provided, for instance SHE PWM. Moreover, the increased share of wind power in

total energy production demands more realistic modelling, including fully controlled AC-

DC-AC high power converter models, so not only the inverter model, but rectifier one can

be simulated further.

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Page 92: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 1 I(VII)

APPENDIX 1: IGBT-module datasheet

Page 93: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 1 II(VII)

Page 94: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 1 III(VII)

Page 95: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 1 IV(VII)

Page 96: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 1 V(VII)

Page 97: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 1 VI(VII)

Page 98: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 1 VII(VII)

Page 99: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 2 I(I)

Appendix 2: General model of NPC and ANPC inverter block diagrams with SVM control

blocks

1

m

50

f

m

f

Out1

Out2

Out3

Out4

Out5

Out6

Out7

Out8

Out9

Out10

Out11

Out12

SVM

PhaseA

PhaseB

PhaseC

Network_load

In1

In2

In3

In4

In5

In6

In7

In8

In9

In10

In11

In12

PhaseA

PhaseB

PhaseC

3-level NPC Inverter

Discrete,Ts = 5e-006 s.

powergui

1

m

50

f

In1

In2

Out1

Out2

Out3

Out4

Out5

Out6

Out7

Out8

Out9

Out10

Out11

Out12

Out13

Out14

Out15

Out16

Out17

Out18

SVM

PhaseA

PhaseB

PhaseC

Network_load

In1

In2

In3

In4

In5

In6

In7

In8

In9

In10

In11

In12

In13

In14

In15

In16

In17

In18

PhaseA

PhaseB

PhaseC

3-level ANPC Inverter

Page 100: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 3 I(I)

Appendix 3: The compound SVM control module

12

Out12

11

Out11

10

Out10

9

Out9

8

Out8

7

Out7

6

Out6

5

Out5

4

Out4

3

Out3

2

Out2

1

Out1

1/(6*6*50)

Ts

In1

In2

In3

In4

In5

Out1

Out2

Out3

Out4

Out5

Out6

Out7

Out8

Out9

Out10

Out11

Out12

Switching_Control

Pulse

T=Ts/10

reg4_t1

Goto9

reg3_t3

Goto8

reg3_t2

Goto7

reg3_t1

Goto6

reg2_t3

Goto5

reg2_t2

Goto4

reg2_t1

Goto3

reg1_t3

Goto2

reg4_t3

Goto11

reg4_t2

Goto10

reg1_t2

Goto1

reg1_t1

Goto

(3^0.5)/2

Gain

f requency

clock

alpha

sector

Definition of angle and sector

m=0.866

alpha

Region1

Region2

Region3

Region4

Definition of Region

Ts

m

alpha

reg1_t1

reg1_t2

reg1_t3

reg2_t1

reg2_t2

reg2_t3

reg3_t1

reg3_t2

reg3_t3

reg4_t1

reg4_t2

reg4_t3

Conducting_Time_Calculator

2

f

1

m

Page 101: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 4 I(I)

Appendix 4: ‘Definition_of_angle_and_sector’ block diagram

Num_vectors

2

sector

1

alpha

0

zero

10

scale_koeff

1/10

scale-koeff

1

increase1

60

degrees_in_sector

floor

Rounding

Function

==

Relational

Operator3

==

Relational

Operator1

>=

Relational

Operator

Product

6

Num_of_sectors

1

u

Math

Function1

1

u

Math

Function

pi/180

Gain2

1/6

Gain

double

double

Count

Up

Inc

Rst

Cnt

Hit

Counter1

Count

Up

Inc

Rst

Cnt

Hit

Counter

50*36

1/Ts

2

clock

1

frequency

Page 102: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 5 I(I)

Appendix 5: ‘Definition_of_Region’ block diagram

m2

4

Region4

3

Region3

2

Region2

1

Region1

sin

Trigonometric

Function2

cos

Trigonometric

Function1

sin

Trigonometric

Function

In1 Out1

Triggered

Subsystem

Scope2

==

<

<

<=

<=

>

>

>

<=

Pulse

T=Ts

Product1

Product

AND

OR

NOT

AND

AND

2/sqrt(3)

Gain1

1/sqrt(3)

Gain

3^0.5/2

Constant4

0.5

Constant3

0.5

Constant2

0.5

Constant1

0.5

Constant

2

alpha

1

m=0.866

m1

Page 103: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 6 I(I)

Appendix 6: ‘Conducting_Time_Calculator’ block diagram

alpha

m

Ts

12

reg4_t3

11

reg4_t2

10

reg4_t1

9

reg3_t3

8

reg3_t2

7

reg3_t1

6

reg2_t3

5

reg2_t2

4

reg2_t1

3

reg1_t3

2

reg1_t2

1

reg1_t1

sin

Trigonometric

Function9

sin

Trigonometric

Function8

sin

Trigonometric

Function7

sin

Trigonometric

Function6

sin

Trigonometric

Function5

sin

Trigonometric

Function4

sin

Trigonometric

Function3

sin

Trigonometric

Function2

sin

Trigonometric

Function1

In1 Out1

Triggered

Subsystem

Pulse

T=Ts

Product9

Product8

Product7

Product6

Product5

Product4

Product3

Product2

Product15

Product14

Product13

Product12

Product11

Product10

Product1

Product

2

Gain9

-2

Gain8

-2

Gain7

2

Gain6

2

Gain5-1

Gain4

2

Gain3

2

Gain2

2

Gain11

-1

Gain10

-2

Gain1

Dead Zone9

Dead Zone8

Dead Zone7

Dead Zone6

Dead Zone5

Dead Zone4

Dead Zone3

Dead Zone2

Dead Zone11

Dead Zone10

Dead Zone1

Dead Zone

1

Constant9

pi/3

Constant8

pi/3

Constant7

1

Constant6

pi/3

Constant5

1

Constant4

pi/3

Constant3

pi/3

Constant2

1

Constant13

pi/3

Constant12

1

Constant11

1

Constant10

1

Constant1

pi/3

Constant

3

alpha

2

m

1

Ts

Page 104: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 7 I(V)

Appendix 7: ‘Switching_Control’ block diagram for NPC inverter and Region2 signal

routing

12

Switch12

11

Switch11

10

Switch10

9

Switch9

8

Switch8

7

Switch7

6

Switch6

5

Switch5

4

Switch4

3

Switch3

2

Switch2

1

Switch1

sector

reg4_state1

reg4_state2

reg4_state3

reg4_state4

Region4

sector

reg3_state1

reg3_state2

reg3_state3

reg3_state4

reg3_state5

Region3

sector

reg2_state1

reg2_state2

reg2_state3

reg2_state4

Region2

sector

reg1_state1

reg1_state2

reg1_state3

reg1_state4

reg1_state5

reg1_state6

reg1_state7

Region1

In1

In2

In3

In4

In5

In6

In7

In8

In9

In10

In11

In12

In13

In14

In15

In16

In17

In18

In19

In20

In21

In22

In23

In24

Switch1

Switch2

Switch3

Switch4

Switch5

Switch6

Switch7

Switch8

Switch9

Switch10

Switch11

Switch12

Final_Logic

reg4_state1

reg4_state2

reg4_state3

reg4_state4

Region4

S1

S2

S3

S4

S5

S6

AND_Mux_block4

reg3_state1

reg3_state2

reg3_state3

reg3_state4

reg3_state5

Region3

S1

S2

S3

S4

S5

S6

AND_Mux_block3

reg2_state1

reg2_state2

reg2_state3

reg2_state4

Region2

S1

S2

S3

S4

S5

S6

AND_Mux_block2

reg1_state1

reg1_state2

reg1_state3

reg1_state4

reg1_state5

reg1_state6

reg1_state7

Region1

S1

S2

S3

S4

S5

S6

AND_Mux_block1

5

In5

4

In4

3

In3

2

In2

1 In1

Page 105: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 7 II(V)

4

reg2_state4

3

reg2_state3

2

reg2_state2

1

reg2_state1

1

2

3

4

5

*, 6

region2_state4

1

2

3

4

5

*, 6

region2_state3

1

2

3

4

5

*, 6

region2_state2

1

2

3

4

5

*, 6

region2_state1

(1 1 1 1 0 0)

PPN1

(1 1 1 1 0 1)

PP0

(1 1 0 0 1 1)

PNP

(1 1 0 0 0 0)

PNN1

(1 1 0 0 0 1)

PN01

(1 1 0 1 1 1)

P0P1

(1 1 0 1 0 0)

P0N

(1 1 0 1 0 1)

P00

(0 0 1 1 1 1)

NPP1

(0 0 1 1 0 0)

NPN1

(0 0 1 1 0 1)

NP0

(0 0 0 0 1 1)

NNP1

(0 0 0 0 0 1)

NN01

(0 0 0 1 1 1)

N0P

(0 0 0 1 0 0)

N0N1

(0 0 0 1 0 1)

N00

(0 1 1 1 1 1)

0PP1

(0 1 1 1 0 0)

0PN1

(0 1 1 1 0 1)

0P0

(0 1 0 0 1 1)

0NP

(0 1 0 0 0 0)

0NN1

(0 1 0 0 0 1)

0N0

(0 1 0 1 1 1)

00P

(0 1 0 1 0 0)

00N

1

sector

Page 106: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 7 III(V)

6

S6

5

S5

4

S4

3

S3

2

S2

1

S1

ramp

t3

t1/2

t2

t1/2_f

t1/2_s

t3F

t2F

Switching sequence Reg2

In1

In2

In3

In4

In5

In6

In7

Out1

Out2

Out3

Out4

Out5

Out6

Subsystem3

In1

In2

In3

In4

In5

In6

In7

Out1

Out2

Out3

Out4

Out5

Out6

Subsystem2

In1

In2

In3

In4

In5

In6

In7

Out1

Out2

Out3

Out4

Out5

Out6

Subsystem1

In1

In2

In3

In4

In5

In6

In7

Out1

Out2

Out3

Out4

Out5

Out6

Subsystem

Pulse

T=Ts

AND

Logical

Operator9

AND

Logical

Operator8

AND

Logical

Operator7

AND

Logical

Operator6

OR

Logical

Operator5

OR

Logical

Operator4

OR

Logical

Operator3

OR

Logical

Operator2

AND

Logical

Operator11

AND

Logical

Operator10

OR

Logical

Operator1

OR

Logical

Operator

1/2

Gain6

reg2_t2

From2

reg2_t3

From1

reg2_t3

From

5

Region2

4

reg2_state4

3

reg2_state3

2

reg2_state2

1

reg2_state1

Page 107: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 7 IV(V)

Forming signals for lower part of NPC topology IGBTs

12

Switch12

11

Switch11

10

Switch10

9

Switch9

8

Switch8

7

Switch7

6

Switch6

5

Switch5

4

Switch4

3

Switch3

2

Switch2

1

Switch1

OR

S6

OR

S5

OR

S4

OR

S3

OR

S2

OR

S1

NOT

Logical

Operator5

NOT

Logical

Operator4

NOT

Logical

Operator3

NOT

Logical

Operator2

NOT

Logical

Operator1

NOT

Logical

Operator

24

In24

23

In23

22

In22

21

In21

20

In20

19

In19

18

In18

17

In17

16

In16

15

In15

14

In14

13

In13

12

In12

11

In11

10

In10

9

In9

8

In8

7

In7

6

In6

5

In5

4

In4

3

In3

2

In2

1

In1

Page 108: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 7 V(V)

‘Switching_Sequence’ for region 2

4

t2F

3

t3F

2

t1/2_s

1

t1/2_f

ScopeAND

ANDAND

NOT

ANDAND

NOT

NOT

In_t

rampOut_t

Form_imp7

In_t

rampOut_t

Form_imp6

In_t

rampOut_t

Form_imp5

In_t

rampOut_t

Form_imp1

4

t2

3

t1/2

2

t3

1

ramp

Page 109: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 8 I(II)

Appendix 8: Three-level NPC and ANPC inverter models with measurement blocks

3

PhaseC

2

PhaseB

1

PhaseA

g CE

S34

g CE

S33

g CE

S32

g CE

S31

g CE

S24

g CE

S23

g CE

S22

g CE

S21

g CE

S14

g CE

S13

g CE

S12

g CE

S11

Is4

Goto9

Is3

Goto8

Is2

Goto7

Is1

Goto6

Id02

Goto5

Id01

Goto4

Id4

Goto3

Id3

Goto2

Cs4

Goto13

Cs3

Goto12

Cs2

Goto11

Cs1

Goto10

Id2

Goto1

Id1

Goto

DC Voltage Source1

DC Voltage Source

D34

D33

D32

D31

D24

D23

D22

D21

D14

D13

D12

D11

D06

D05

D04

D03

D02

D01

i+

-

Cd4

i+

-

Cd3

i+

-Cd2

i+

-

Cd1

i+

-

Cd02

i+

-

Cd01

i+

-

CS4

i+

-

CS2

i+

-

CS1i

+-

C

12

In12

11

In11

10

In10

9

In9

8

In8

7

In7

6

In6

5

In5

4

In4

3

In3

2

In2

1

In1

Page 110: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 8 II(II)

3

PhaseC

2

PhaseB

1

PhaseA

Scope

g CE

S36

g CE

S35

g CE

S34

g CE

S33

g CE

S32

g CE

S31

g CE

S26

g CE

S25

g CE

S24

g CE

S23

g CE

S22

g CE

S21

g CE

S16

g CE

S15

g CE

S14

g CE

S13

g CE

S12

g CE

S11

i+

-

Is6

i+

-

Is5

i+

-

Is4

i+

-

Is3

i+

-

Is2

i+

-

Is1

i+

-

Id4

i+

-

Id3

i+

-

Id2

i+

-

Id1

i+

-

Id02

i+

-

Id01

Id4

Goto9

Id3

Goto8

Id2

Goto7

Id1

Goto6

Is6

Goto5

Is5

Goto4

Is4

Goto3

Is3

Goto2

CS6

Goto17

CS5

Goto16

CS4

Goto15

CS3

Goto14

CS2

Goto13

CS1

Goto12

Id5

Goto11

Id6

Goto10

Is2

Goto1

Is1

Goto

DC Voltage Source1

DC Voltage Source

D34

D33

D32

D31

D24

D23

D22

D21

D14

D13

D12

D11

D06

D05

D04

D03

D02

D01

18

In18

17

In17

16

In16

15

In15

14

In14

13

In13

12

In12

11

In11

10

In10

9

In9

8

In8

7

In7

6

In6

5

In5

4

In4

3

In3

2

In2

1

In1

Page 111: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 9 I(I)

Appendix 9: m-file with simulation parameters and base vectors arrays declaration for

NPC and ANPC models

clc; clear all; % Switching states for one phase a...f=[s1 s2 s3 s4 s5 s6]. % States a and f give fully positive and negative voltages for one phase, % respectively, and create paths for positive and negative currents, % whereas states b,c,d and e create alternative paths for current flow % in the middle point of ANPC topology.

a=[1 1 0 0 0 1]; b=[0 1 0 0 1 0]; c=[0 1 0 1 1 0]; d=[1 0 1 0 0 1]; e=[0 0 1 0 0 1]; f=[0 0 1 1 1 0];

% Parameters of the model and load m=3; % number of phases init_t=1e-9; %losses calculation Cur_rise_tol=4; %assumptions A_Cur_rise_tol=20; Time_sat_limit=2e-5; Tf=1/50; % Fundamental period [s] Tsw=1/(50*36); % Switching period [s] tolerance=0; % min pulse length [s] Udc=2.8e+3; % DC-link voltage [V] Rload=1; % Load resistance [Ohm] Lload=2e-3; % Load inductance [H]

% Parameters of IGBTs and diodes used in calculation model Tail_time=0.0000002; % Rise time [s] Fall_time=0.0000002; % Fall time [s] RGin=0.42; Ldcl=0; uCEO=1.9; % IGBT threshold voltage [V] rC=0.002; % IGBT on-state resistance [Ohm] uDO=1.4; % Diode threshold voltage [V] rD=0.0023; % Diode on-state resistance [Ohm] Irated=1200; % Rated current from the datasheet [A] Urated=1650; % Rated voltage from the datasheet[V] Eon=2.2; % Turn-on energy loss [J] Eoff=1.55; % Turn-off energy loss [J] Erec=1.55; % Recovery energy loss [J]

sim('ANPC_final.mdl'); sim('NPC_final.mdl');

Page 112: LAPPEENRANTA UNIVERSITY OF TECHNOLOGY LUT Energy

APPENDIX 10 I(I)

Appendix 10: Currents of symmetrical components Sx1, Sx4 and Sx2, Sx3 simultaneously

conducting Dx1 and Dx2 for NPC inverter.